md-80 maintenance manualevertsair.com/vendors/md80mm.pdfmd-80 maintenance manual md-80 maintenance...
TRANSCRIPT
COV-1
MD-80 MAINTENANCE MANUAL
MD-80 MAINTENANCE MANUAL
THIS MANUAL IS THE PROPERTY OF EVERTS AIR CARGO
The person, or office, this manual has been assigned to will be responsible for the general maintenance and
insertion of revisions.
This document has EAR data with Export Control Classification Numbers (ECCN) of:
9E991
Export of this technology is controlled under the United States Export Administration Regulations (EAR) (15 CFR 730-774). An export license may be required before it is used for development, production or use by foreign persons from specific countries. The controller of this data has the individual responsibility to abide by all export laws.
BOEING PROPRIETARY, CONFIDENTIAL, AND/OR TRADE SECRET
Copyright 2010 The Boeing Company
Unpublished Work - All Rights Reserved
Boeing claims copyright in each page of this document only to the extent that the page contains copyright-able subject matter. Boeing also claims copyright in this document as a compilation and/or collective work.
This document includes proprietary information owned by The Boeing Company and/or one of more third parties. Treatment of the document and the information it contains is governed by contract with Boeing. For more information, contact The Boeing Company, P.O. Box 3707, Seattle, Washington 98124.
Boeing, the Boeing signature, the Boeing symbol, 707, 717, 727, 737, 747, 757, 767, 777, 787, Dreamliner, BBJ, DC-8, DC-9, DC-10, KC-10, KDC-10, MD-10, MD-11, MD-80, MD-90, P-8A, Poseidon and the Boeing livery are all trademarks owned by The Boeing Company; and no trademark license is granted in connection with this document unless provided in writing by Boeing.
MANUAL NUMBER ___________________________
ASSIGNED TO ___________________________
POSITION ___________________________
DATE ___________________________
Rev 0 19 March 2014
COV-2
MD-80 MAINTENANCE MANUAL
Intentionally Left Blank
Rev 0 19 March 2014
LEP-1
List of Effective Pages
Ch. # Page # Revision & Date (mm/dd/yyyy) Ch. # Page # Revision & Date (mm/dd/yyyy)
MD-80 MAINTENANCE MANUAL
COV 1 Rev 0 03/19/2014COV 2 Rev 0 03/19/2014LEP 1 Rev 0 03/19/2014LEP 2 Rev 0 03/19/2014LEP 3 Rev 0 03/19/2014LEP 4 Rev 0 03/19/2014TOC 1 Rev 0 03/19/2014TOC 2 Rev 0 03/19/2014TOC 3 Rev 0 03/19/2014TOC 4 Rev 0 03/19/2014INTRO 1 Rev 0 03/19/2014INTRO 2 Rev 0 03/19/2014INTRO 3 Rev 0 03/19/2014INTRO 4 Rev 0 03/19/2014INTRO 5 Rev 0 03/19/2014INTRO 6 Rev 0 03/19/20141 1 Rev 0 03/19/20141 2 Rev 0 03/19/20141 3 Rev 0 03/19/20141 4 Rev 0 03/19/20142 1 Rev 0 03/19/20142 2 Rev 0 03/19/20142 3 Rev 0 03/19/20142 4 Rev 0 03/19/20142 5 Rev 0 03/19/20142 6 Rev 0 03/19/20142 7 Rev 0 03/19/20142 8 Rev 0 03/19/20142 9 Rev 0 03/19/20142 10 Rev 0 03/19/20142 11 Rev 0 03/19/20142 12 Rev 0 03/19/20142 13 Rev 0 03/19/20142 14 Rev 0 03/19/20142 15 Rev 0 03/19/20142 16 Rev 0 03/19/20142 17 Rev 0 03/19/2014
2 18 Rev 0 03/19/20142 19 Rev 0 03/19/20142 20 Rev 0 03/19/20142 21 Rev 0 03/19/20142 22 Rev 0 03/19/20142 23 Rev 0 03/19/20142 24 Rev 0 03/19/20142 25 Rev 0 03/19/20142 26 Rev 0 03/19/20142 27 Rev 0 03/19/20142 28 Rev 0 03/19/20142 29 Rev 0 03/19/20142 30 Rev 0 03/19/20142 31 Rev 0 03/19/20142 32 Rev 0 03/19/20142 33 Rev 0 03/19/20142 34 Rev 0 03/19/20142 35 Rev 0 03/19/20142 36 Rev 0 03/19/20142 37 Rev 0 03/19/20142 38 Rev 0 03/19/20143 1 Rev 0 03/19/20143 2 Rev 0 03/19/20143 3 Rev 0 03/19/20143 4 Rev 0 03/19/20143 5 Rev 0 03/19/20143 6 Rev 0 03/19/20143 7 Rev 0 03/19/20143 8 Rev 0 03/19/20143 9 Rev 0 03/19/20143 10 Rev 0 03/19/20143 11 Rev 0 03/19/20143 12 Rev 0 03/19/20143 13 Rev 0 03/19/20143 14 Rev 0 03/19/20143 15 Rev 0 03/19/20143 16 Rev 0 03/19/2014
Rev 0 19 March 2014
LEP-2
List of Effective Pages
Ch. # Page # Revision & Date (mm/dd/yyyy) Ch. # Page # Revision & Date (mm/dd/yyyy)
MD-80 MAINTENANCE MANUAL
3 17 Rev 0 03/19/20143 18 Rev 0 03/19/20143 19 Rev 0 03/19/20143 20 Rev 0 03/19/20143 21 Rev 0 03/19/20143 22 Rev 0 03/19/20143 23 Rev 0 03/19/20143 24 Rev 0 03/19/20143 25 Rev 0 03/19/20143 26 Rev 0 03/19/20143 27 Rev 0 03/19/20143 28 Rev 0 03/19/20144 1 Rev 0 03/19/20144 2 Rev 0 03/19/20144 3 Rev 0 03/19/20144 4 Rev 0 03/19/20144 5 Rev 0 03/19/20144 6 Rev 0 03/19/20144 7 Rev 0 03/19/20144 8 Rev 0 03/19/20144 9 Rev 0 03/19/20144 10 Rev 0 03/19/20144 11 Rev 0 03/19/20144 12 Rev 0 03/19/20144 13 Rev 0 03/19/20144 14 Rev 0 03/19/20145 1 Rev 0 03/19/20145 2 Rev 0 03/19/20145 3 Rev 0 03/19/20145 4 Rev 0 03/19/20145 5 Rev 0 03/19/20145 6 Rev 0 03/19/20145 7 Rev 0 03/19/20145 8 Rev 0 03/19/20145 9 Rev 0 03/19/20145 10 Rev 0 03/19/20145 11 Rev 0 03/19/2014
5 12 Rev 0 03/19/20145 13 Rev 0 03/19/20145 14 Rev 0 03/19/20145 15 Rev 0 03/19/20145 16 Rev 0 03/19/20145 17 Rev 0 03/19/20145 18 Rev 0 03/19/20145 19 Rev 0 03/19/20145 20 Rev 0 03/19/20145 21 Rev 0 03/19/20145 22 Rev 0 03/19/20146 1 Rev 0 03/19/20146 2 Rev 0 03/19/20146 3 Rev 0 03/19/20146 4 Rev 0 03/19/20146 5 Rev 0 03/19/20146 6 Rev 0 03/19/20146 7 Rev 0 03/19/20146 8 Rev 0 03/19/20146 9 Rev 0 03/19/20146 10 Rev 0 03/19/20146 11 Rev 0 03/19/20146 12 Rev 0 03/19/20146 13 Rev 0 03/19/20146 14 Rev 0 03/19/20146 15 Rev 0 03/19/20146 16 Rev 0 03/19/20146 17 Rev 0 03/19/20146 18 Rev 0 03/19/20146 19 Rev 0 03/19/20146 20 Rev 0 03/19/20146 21 Rev 0 03/19/20146 22 Rev 0 03/19/20146 23 Rev 0 03/19/20146 24 Rev 0 03/19/20147 1 Rev 0 03/19/20147 2 Rev 0 03/19/2014
Rev 0 19 March 2014
LEP-3
List of Effective Pages
Ch. # Page # Revision & Date (mm/dd/yyyy) Ch. # Page # Revision & Date (mm/dd/yyyy)
MD-80 MAINTENANCE MANUAL
8 1 Rev 0 03/19/20148 2 Rev 0 03/19/20149 1 Rev 0 03/19/20149 2 Rev 0 03/19/201410 1 Rev 0 03/19/201410 2 Rev 0 03/19/201410 3 Rev 0 03/19/201410 4 Rev 0 03/19/201410 5 Rev 0 03/19/201410 6 Rev 0 03/19/201411 1 Rev 0 03/19/201411 2 Rev 0 03/19/201412 1 Rev 0 03/19/201412 2 Rev 0 03/19/201412 3 Rev 0 03/19/201412 4 Rev 0 03/19/201412 5 Rev 0 03/19/201412 6 Rev 0 03/19/201412 7 Rev 0 03/19/201412 8 Rev 0 03/19/201412 9 Rev 0 03/19/201412 10 Rev 0 03/19/201412 11 Rev 0 03/19/201412 12 Rev 0 03/19/201412 13 Rev 0 03/19/201412 14 Rev 0 03/19/201412 15 Rev 0 03/19/201412 16 Rev 0 03/19/201412 17 Rev 0 03/19/201412 18 Rev 0 03/19/201412 19 Rev 0 03/19/201412 20 Rev 0 03/19/201412 21 Rev 0 03/19/201412 22 Rev 0 03/19/201412 23 Rev 0 03/19/201412 24 Rev 0 03/19/201412 25 Rev 0 03/19/2014
12 26 Rev 0 03/19/201412 27 Rev 0 03/19/201412 28 Rev 0 03/19/201412 29 Rev 0 03/19/201412 30 Rev 0 03/19/201412 31 Rev 0 03/19/201412 32 Rev 0 03/19/201412 33 Rev 0 03/19/201412 34 Rev 0 03/19/201412 35 Rev 0 03/19/201412 36 Rev 0 03/19/201412 37 Rev 0 03/19/201412 38 Rev 0 03/19/201412 39 Rev 0 03/19/201412 40 Rev 0 03/19/2014Appendix A LEP1 Rev 0 03/19/2014Appendix A LEP2 Rev 0 03/19/2014Appendix A LEP3 Rev 0 03/19/2014Appendix A LEP4 Rev 0 03/19/2014
Rev 0 19 March 2014
LEP-4
MD-80 MAINTENANCE MANUAL
Intentionally Left Blank
Rev 0 19 March 2014
TOC-1
Table of Contents
MD-80 MAINTENANCE MANUAL
Preface - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -INTRO-1
Chapter 1 Introduction - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 1-1
1.1 General - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 1-11.2 Effectivity - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 1-11.3 Purpose - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 1-11.4 Maintenance Tasks - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 1-21.5 Main Cargo Door Modification - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 1-21.6 Aircraft Storage- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 1-3
Chapter 2 Systems and Powerplant Program - - - - - - - - - - - - - - - - - - - - - - - - - 2-1
2.1 Scope - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 2-12.2 General Notes - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 2-12.3 Notes: Main Cargo Door Modification (STC ST02434LA) - - - - - - - - - - - - - - - - - - - - - - - - 2-12.4 Systems and Powerplant Program - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 2-2
2.4.1 DFDR Maintenance Program (14 CFR Part 121.344(a)(b)(c)) - - - - - - - - - - - - - - - - - - 2-22.4.1.1 General - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 2-22.4.1.2 System Description - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 2-22.4.1.3 Scheduled Maintenance Tasks- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 2-32.4.1.4 Data Conversion SSDFDR - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 2-32.4.1.5 Functional Checks- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 2-32.4.1.6 Underwater Locator Device (ULD) - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 2-32.4.1.7 Correlation Requirements- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 2-32.4.1.8 Accessing Online References - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 2-3
2.5 Notes: ATA 49 (APU) - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 2-42.6 Notes: ATA 71-80 (Powerplant) - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 2-4
Figure 2-A: Systems and Powerplant Maintenance Program Example Page - - - - - - - - - - - - - 2-52.7 Page Format Explanation - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 2-6
Chapter 3 Structural Maintenance Program - - - - - - - - - - - - - - - - - - - - - - - - - - 3-1
3.1 Scope - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 3-13.2 Notes: Main Cargo Door Modification (STC ST02434LA) - - - - - - - - - - - - - - - - - - - - - - - - 3-13.3 Notes- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 3-1
3.3.1 Inspection Task Definitions - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 3-13.3.1.1 Inspection - General Visual- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 3-13.3.1.2 Inspection - Detailed - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 3-13.3.1.3 Inspection - Special Detailed- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 3-2
3.4 Operating Rules - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 3-23.5 Fatigue Related Inspection Program - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 3-23.6 Corrosion Prevention and Control Requirements - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 3-23.7 Corrosion Prevention and Control Program - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 3-33.8 Corrosion Level Definition - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 3-4
3.8.1 Corrosion Level 1 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 3-43.8.2 Corrosion Level 2 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 3-43.8.3 Corrosion Level 3 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 3-4
3.9 Reporting Results of Structural Inspections - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 3-4Figure 3-A: Structures Maintenance Program Example Page - - - - - - - - - - - - - - - - - - - - - - - 3-5
3.10 Page Format Explanation - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 3-6
Rev 0 19 March 2014
TOC-2
Table of Contents
MD-80 MAINTENANCE MANUAL
Chapter 4 Zonal Inspection Program (ZIP) - - - - - - - - - - - - - - - - - - - - - - - - - - -4-1
4.1 Scope - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 4-14.2 Notes - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 4-14.3 Notes: Main Cargo Door Modification (STC ST02434LA) - - - - - - - - - - - - - - - - - - - - - - - - 4-14.4 Zonal Program Rules- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 4-1
Figure 4-A: Zonal Maintenance Program Example Page- - - - - - - - - - - - - - - - - - - - - - - - - - 4-34.5 Task Summary Page Format- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 4-4
Chapter 5 Source Documents for Tasks - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -5-1
5.1 Scope - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 5-1
Chapter 6 Weight and Balance Procedures- - - - - - - - - - - - - - - - - - - - - - - - - - - -6-1
6.1 Policies - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 6-16.1.1 General - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 6-16.1.2 Responsibilities - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 6-16.1.3 Controlling Documents - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 6-1
6.2 Weight and Balance Control- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 6-16.2.1 Individual Aircraft Weight and Balance Control - - - - - - - - - - - - - - - - - - - - - - - - - - - 6-16.2.2 Responsibility - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 6-1
6.3 Terms and Definitions - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 6-26.3.1 Arm - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 6-26.3.2 Center of Gravity (CG) - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 6-26.3.3 Center of Gravity Limits - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 6-26.3.4 Center of Gravity Range - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 6-26.3.5 Datum (REF. Datum) - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 6-26.3.6 Equipment Check List - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 6-26.3.7 Required Equipment List - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 6-26.3.8 Moment - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 6-26.3.9 Moment Index (or Index)- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 6-36.3.10 Station - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 6-36.3.11 Basic Weight - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 6-36.3.12 Empty Weight - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 6-36.3.13 Basic Operating Weight - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 6-36.3.14 Basic Operating Index - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 6-36.3.15 Operating Index - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 6-3
6.4 Weight and Balance Forms: M-9, M-9A, M-9B, M-9E, M-9G, and M-9H - - - - - - - - - - - - - - 6-36.4.1 Pre-Weighing Check List (Form M-9) - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 6-36.4.2 Aircraft Equipment List (Form M-9B) - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 6-36.4.3 Aircraft Actual Weight and Balance (Form M-9): - - - - - - - - - - - - - - - - - - - - - - - - - - 6-36.4.4 Accumulative Weight Change Record (Form M-9G) - - - - - - - - - - - - - - - - - - - - - - - - 6-46.4.5 Change to Basic Operating Weight (BOW) (Form M-9H)- - - - - - - - - - - - - - - - - - - - - 6-4
6.5 Preweighing Checklist - Form M-9A - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 6-76.6 Form M-9E - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 6-96.7 Accumulative Weight Change Record (Form M-9G) - - - - - - - - - - - - - - - - - - - - - - - - - - - 6-106.8 Change to Basic Operating Weight (BOW) Form M-9H - - - - - - - - - - - - - - - - - - - - - - - - - 6-116.9 Aircraft Equipment List - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 6-12
Chapter 7 Reserved for Future Use - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -7-1
Rev 0 19 March 2014
TOC-3
Table of Contents
MD-80 MAINTENANCE MANUAL
Chapter 8 Reserved for Future Use - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 8-1
Chapter 9 Reserved for Future Use - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 9-1
Chapter 10 Airworthiness Limitations Instructions,Certification Maintenance Requirements,Special Compliance Items- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 10-1
10.1 Introduction - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 10-110.2 Notes: Main Cargo Door Modification (STC ST02434LA)- - - - - - - - - - - - - - - - - - - - - - - 10-110.3 Scope- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 10-110.4 Airworthiness Limitations Instructions (ALI) - Systems- - - - - - - - - - - - - - - - - - - - - - - - - 10-1
10.4.1 Fuel Systems Airworthiness Limitations - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 10-110.5 Certification Maintenance Requirements (CMR) - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 10-2
10.5.1 Selection of CMRs- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 10-210.5.2 CMR Definition - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 10-2
10.6 Post-Certification Changes to CMRs- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 10-310.7 Special Compliance Items (SCI)- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 10-4
10.7.1 Introduction - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 10-410.7.2 Definition- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 10-5
Chapter 11 Reserved for Future Use- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 11-1
Chapter 12 STC - Instructions for Continued Airworthiness - - - - - - - - - - - - - 12-1
12.1 Maintenance Planning Data Document Supplement for MD-80 Cargo Conversion (STC ST02434LA) - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 12-1
Figure 12-A: Systems Maintenance Program Example Page - - - - - - - - - - - - - - - - - - - - - - 12-112.2 Structural Maintenance Program - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 12-13
Figure 12-B: Structural Maintenance Program Example Page - - - - - - - - - - - - - - - - - - - - 12-14Figure 12-C: Structural Maintenance Program Tasks - - - - - - - - - - - - - - - - - - - - - - - - - - 12-16
12.3 Zonal Inspection Program - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 12-20Figure 12-D: Zonal Inspection Program Tasks - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 12-20
12.4 Supplemental Structural Inspection Items for MD-80 Aircraft Modifiedwith Freighter Conversion STC. No. ST02434LA(Fatigue Related Inspections) - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 12-20
Figure 12-E: Douglas NDTSPM, MDC 93K0393, Part 06 Inspection MethodsReference Table - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 12-21
Figure 12-F: Supplemental Structural Inspection Tasks for MD-80 AircraftModified with Freighter Conversion STC No. ST02434LA(Fatigue Related Inspections) - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 12-22
12.5 Inspection Instructions for VAI 9G Barrier Installation, DC-9-80 and MD-88 Aircraft - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 12-32
Figure 12-G: Douglas NDTSPM, MDC93K0393, Part 06 Inspection MethodsReference Table - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 12-32
Figure 12-H: VAI 9G Barrier Installation Inspection Tasks - - - - - - - - - - - - - - - - - - - - - - 12-3212.6 Cargo Loading System - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 12-33
12.6.1 General Description of Cargo Loading System - - - - - - - - - - - - - - - - - - - - - - - - - - 12-3312.6.2 MDCLS Functionality and Subcomponents - - - - - - - - - - - - - - - - - - - - - - - - - - - - 12-3312.6.3 Airworthiness Limitations- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 12-34
Rev 0 19 March 2014
TOC-4
Table of Contents
MD-80 MAINTENANCE MANUAL
12.6.4 Placards - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 12-3412.6.5 Cleaning - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 12-3412.6.6 Inspections - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 12-3412.6.7 Applicable Wear Tolerances- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 12-3512.6.8 Corrosion - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 12-3612.6.9 Component Removal and Installation- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 12-3612.6.10 Torque Requirements- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 12-3612.6.11 Storage Instructions- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 12-3612.6.12 Lubrication - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 12-3612.6.13 EWIS Impact - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 12-36Figure 12-I: ANCRA MD-80 Cargo Loading System Tasks - - - - - - - - - - - - - - - - - - - - - 12-37
12.7 ARTEX C406-1 Emergency Locator Transmitter (ELT) System - - - - - - - - - - - - - - - - - 12-37Figure 12-J: ELT Maintenance & Inspection Tasks - - - - - - - - - - - - - - - - - - - - - - - - - - - 12-38
12.8 ELT Installation Structural Inspection Requirements - - - - - - - - - - - - - - - - - - - - - - - - - 12-38Figure 12-K: Structural Inspection Requirements Tasks - - - - - - - - - - - - - - - - - - - - - - - - 12-39
Appendix A- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -Appendix A-1
Rev 0 19 March 2014
INTRO-1
MD-80 MAINTENANCE MANUAL
PREFACE
This manual remains the property of Everts Air Cargo.
As required by, Title 14 CFR Part 121.137, the person to whom this manual is issued shall be responsible for keeping the manual in usable form and in current condition, inserting revisions when received and recording insertion dates on the revision control page.
This manual must be returned to Everts Air Cargo Maintenance Office in the event of termination of employment.
This manual contains instructions, information and data necessary to guide operations personnel in the performance of their assigned duties with the highest degree of safety possible.
All information contained herein is in accordance with the various FARs pertaining thereto and as required by the provisions of Title 14 CFR Parts 119 and 121: Certification and Operations: Domestic, Flag and Supplemental Air Carriers and Commercial Operators of Large Aircraft. This manual must be used in conjunction with the FAR's which are referenced throughout the manual. In the event there appears to be a conflict between this manual and the FAR’s, the regulations will preside.
The company will issue a copy of this manual to company employees and such other persons as may be required to ensure the proper performance of their duties and functions. The company will provide revision service for its manual holders to keep them in current status. Each manual holder is responsible for keeping his copy up to date with the revision service provided.
Revision procedures for all Everts Air Cargo manuals are found in the GOM, Volume I, Chapter 1, Page 1.
Whenever a revision is issued, the revisions will be numbered consecutively for each volume and will indicate the volume affected by the revision material. The revision letter will contain instructions for adding, removing and replacing revised pages.
Upon completion of the revision, the old pages will be destroyed and the person making the revision will enter the date and his name, for the appropriate revision on the Revision Record page located in the front of the affected volume.
Errors or comments regarding the content of this manual should be brought to the attention of the Director of Maintenance.
Everts Air Cargo is referred to as the abbreviation EAC throughout this manual.
Rev 0 19 March 2014
INTRO-2
MD-80 MAINTENANCE MANUAL
Intentionally Left Blank
Rev 0 19 March 2014
INTRO-3
MD-80 MAINTENANCE MANUAL
Revision RecordsMAKE ENTRIES WHEN INSERTING REVISIONS IN THIS MANUAL.
REVISION NO BY DATE REVISION NO BY DATE
Rev 0 19 March 2014
INTRO-4
MD-80 MAINTENANCE MANUAL
Intentionally Left Blank
Rev 0 19 March 2014
INTRO-5
MD-80 MAINTENANCE MANUAL
Tatonduk Outfitters Limited Revision Transmittal Sheet
The following revisions apply to your EVERTS AIR CARGO MD-80 MAINTENANCE MANUAL, dated April 24, 2013. These changes have been incorporated into the Everts Air electronic manual system. Please review the changes below.
14 CFR REGULATIONS REQUIRE THAT COMPANY MANUALS BE MAINTAINED CURRENT. MANUAL HOLDERS NEED TO SIGN BELOW. YOUR SIGNATURE ATTESTS THAT YOU HAVE RECEIVED, REVIEWED, UNDERSTAND, AND INSERTED THIS REVISION.
REPLACED PAGES WILL BE DESTROYED.
NAME OF MANUAL HOLDER/USER __________________________________MANUAL # _______
SIGNATURE OF MANUAL HOLDER/USER _____________________________ DATE __________
UPON COMPLETION, MAIL/FAX TO:
EVERTS AIR CARGOPUBLICATIONSP.O. BOX 61680FAIRBANKS, AK 99706 907-450-2300
REVISION NUMBERDATE
CHAPTER PAGE DESCRIPTION OF CHANGES INSTRUCTIONS
For future reference it is recommended that you copy this page.
Rev 0 19 March 2014
INTRO-6
MD-80 MAINTENANCE MANUAL
Intentionally Left Blank
Rev 0 19 March 2014
1-1
MD-80 MAINTENANCE MANUAL
CHAPTER 1: INTRODUCTION
1.1 General
The Everts Air Cargo (here after known as Everts) DC-9-80SF listed below, shall be maintained in an air-worthy condition in accordance with the inspections and procedures outlined in this maintenance program, the approved Boeing technical manuals, standard practices, and in accordance with Title 14 CFR § 91 Sub-part E. Maintenance, Preventive Maintenance, and Alterations.
This MPD is to be considered as the Manufacturer’s Recommended Maintenance program for the aircraft listed in section 1.2 of this chapter while being operated by Everts as required in Title 14 CFR § 121.367.
The aircraft structure, power plants, systems, and components are to be inspected and serviced periodi-cally, not to exceed the time intervals mentioned in this maintenance program.
The Everts DC-9-80SF Maintenance Planning Data (MPD) document is considered a “Living Document”, in that it will be revised to assure that the aircraft continues to be maintained in an airworthy condition. This will be accomplished through revision procedures.
1.2 Effectivity
This Maintenance Planning Data (MPD) document report ME80-020-TNK is valid for the DC-9-80SF air-craft operated by Everts.
Instructions for use of this MPD document are contained in this chapter under “Description”. Maintenance task instructions are provided in task card format. Task cards are organized in ATA order for each chapter as appropriate.
Irrespective of the type of operational environment, the limitations that are described and specified in the Maintenance Specification Document will be adhered to as applicable to the following Aircraft:
NOTE: Everts Air Cargo aircraft serial number 49470 is considered a DC-9-82SF following the STC freighter conversion However, for MPD purposes DC-9-80SF, DC-9-82SF, and MD-80 are used interchangeably.
The aircraft and its component parts, accessories, and appliances shall be maintained in an airworthy con-dition in accordance with the maximum time limits, as authorized in this document for the accomplishment of the maintenance tasks, periodic inspections, and routine checks. The Maintenance Program will be accomplished using the specific maintenance task cards and the MD-80 Aircraft Maintenance Manual (AMM).
1.3 Purpose
This Everts DC-9-80SF Maintenance Planning Data (MPD) document provides maintenance planning information necessary for the Everts DC-9–80SF. This document lists all Boeing recommended scheduled maintenance tasks and satisfies the requirement that the aircraft have a current inspection program cur-rently recommended by the manufacturer of the airplane per Title 14 CFR § 91.409(f)(3).
This maintenance program ensures that the Everts aircraft and all of its parts can perform their intended functions and reflects three specific program objectives that provide the highest possible level of safety in air transportation.
• The Everts aircraft is released to service is airworthy and has been properly maintained for operations in air transportation.
A/C Registration Model Fuselage No. Manufacturer S/N Eff CodeN73444 DC-9-82 1417 49470 201
Rev 0 19 March 2014
1-2
MD-80 MAINTENANCE MANUAL
• Maintenance and alterations that Everts performs, or that other persons perform for Everts, are per-formed in accordance with the Everts requirements; and
• Competent personnel with adequate facilities and equipment perform maintenance and alterations on the Everts aircraft.
Periodic (scheduled) maintenance tasks outlined in this document may include, but are not limited to, the following sources:
• MD-80 FAA Maintenance Review Board (MRB) Report (ME-MRB-80) - Latest Revision.
• Boeing DC-9 and MD-80 Service Bulletins (SB)*.
• Boeing DC-9 and MD-80 Service Letters (SL)*.
• DC-9 and MD-80 FAA Airworthiness Directives (AD’s)*.
• DC-9 / MD-80 / MD-90 / 717 Special Compliance Item (MDC-92K9145).
• MD-80 Maintenance Implementation Document (MID) (ME80-0016).
• Maintenance Planning Data Document Supplement for MD-80 Cargo Conversion (R-867).
• Supplement to McDonnell Douglas Document No. L-26-022 Supplemental Inspection Document (SIE-367-601).
• Inspection Instructions for: VAI 9G Barrier Installation, DC-9-80 and MD-88 Aircraft (SIE-367-602).
• Instructions for Continued Airworthiness Cargo Loading System Part Number 85130-10,-11, & -12 Installed on MD-80 Freighter (Report No. 9682).
NOTE: This program meets the requirements of Title 14 CFR 121 Subpart AA – AIRWORTHI-NESS AND SAFETY IMPROVEMENTS.
NOTE: *Service Letters, Service Bulletins and Airworthiness Directives are reviewed by Everts and integrated into the maintenance plan where applicable.
1.4 Maintenance Tasks
Utilization Parameter Limits: This program is a Low Utilization Maintenance Program (LUMP) developed by Boeing for Everts. The intervals contained in this document are based on a utilization not to exceed 1,200 FH per year. If the utilization is to exceed 1,200 FH per year then the intervals will need to be re-ana-lyzed and adjusted accordingly.
Many of the scheduled maintenance tasks listed in this document identify the frequency of accomplish-ment in terms of a usage parameter and frequency.
1. Maintenance task intervals.
Check Interval
A 6 Months
C 24 Months
a. In the event the aircraft exceeds the A or C check interval period, (up to a maximum of 10 percent, with a maximum of 90 days) the aircraft will be allowed to fly directly to the maintenance facility where the maintenance is to be performed. The aircraft may make technical stops as needed enroute to the maintenance facility. Everts will inform the Flight Standards District Office (FSDO) in the event this extension is used.
1.5 Main Cargo Door Modification
For a listing of the Instructions for Continued Airworthiness (ICA) for the Aeronautical Engineers, Inc. (AEI) freighter conversion per STC ST02434LA, refer to Chapter 12 of this document.
Rev 0 19 March 2014
1-3
MD-80 MAINTENANCE MANUAL
1.6 Aircraft Storage
1. Procedures.
The procedures found in the MD-80 AMM ATA chapter 05 as well as the engine and APU manuals, will be used of for all levels of aircraft storage.
2. Clock Stoppage.
When an aircraft is placed in storage, maintenance or modification, accumulation of calendar time for the maintenance program scheduled maintenance checks may be halted by taking appropriate procedures and parking the aircraft in an environment not likely to promote corrosion. This is referred to as “Clock Stop-page”. Exceptions to clock stoppage are AD’s and Life Limited Items/Parts. The Zonal and Structures Pro-gram that are specified under Calendar Limits may be halted providing that the storage is per the appropriate manuals. Note that clock stoppage limits for the Zonal and Structures Program per this guide-line are not to exceed 24 Months. The clock stoppage will continue until storage/modifications are com-pleted, appropriate actions are complied with, and the conditions for flight and return to service have been met.
3. Storage.
Any aircraft that has been placed in storage, with proper preservation methods, will have the clock stop-page at the time the preservation for storage is completed. Aircraft that will not be operated for a period of 30 to 90 days may be placed is short term storage. Aircraft that are placed in storage for longer than 90 days may be placed is long term storage. Aircraft that have been placed in short term storage need only have the de-preservation tasks and a complete preflight performed. Aircraft that have been in long term storage will have de-preservation task performed per the OEM's manuals, complete the all “A” checks, landing gear and flight control lubrication tasks performed, and a complete preflight check prior to return-ing aircraft to service.
4. Modification/Repair.
Aircraft that are placed into an extensive modification or repair that will go beyond 60 days may also have the clock stopped at the time the aircraft begins the modification or repair. If the modification or repair is to go beyond 90 days, then considerations will be given to preserving various parts and/or areas of the aircraft that are not going to receive attention during the modification or repair. Aircraft that have been placed out of service for maintenance and/or modification will complete a 1A Check with 2A Landing Gear and 4A check, flight control lubrication tasks, a complete preflight check, and performed applicable de-preserva-tion tasks per OEM manuals, prior to returning aircraft to service.
Rev 0 19 March 2014
1-4
MD-80 MAINTENANCE MANUAL
Intentionally Left Blank
Rev 0 19 March 2014
2-1
MD-80 MAINTENANCE MANUAL
CHAPTER 2: SYSTEMS AND POWERPLANT PROGRAM
2.1 Scope
This chapter of the MPD outlines the scheduled maintenance tasks for the Systems Maintenance Program. This chapter, arranged in ATA order, may cover the following aircraft systems:
2.2 General Notes
1. The terms “check” and “inspection” are not intended to imply a level of skill required to accomplish a task.
2. The phrase “... mechanical control path ...” is used in describing certain scheduled maintenance tasks. This is not intended to include cables, but only components/assemblies required to initiate and termi-nate action.
3. Excessive dust, debris, or overspray of corrosion inhibiting compounds, found during any inspection, is considered to be unsatisfactory condition possibly reducing the fire resistance of the airplane design. Cleanup of these materials should be a standard part of maintenance activity.
4. Certification Maintenance Requirement - CMR. Maintenance requirements arising from aircraft certi-fication activities are described in FAR 25.1309 and AC 25.1309-1. Independent of the MSG-3 analy-sis process, CMRs are developed as part of the aircraft systems safety analyses required for aircraft certification. CMR tasks are identified when system probabilities and failure effects are not expected to be within an acceptable range without a periodic maintenance requirement. All CMR tasks includ-ing CMR task frequencies are controlled in the Certification Maintenance Requirements (CMRs) doc-ument number MDC-J1271approved by FAA Engineering Part 25.
5. A complete set of MPD/MRB/Task Card Number cross-reference indexes can be found in Appendix D.
2.3 Notes: Main Cargo Door Modification (STC ST02434LA)
1. Scheduled maintenance tasks for the main cargo door modification can be found in Chapter 12.
12
20
21
22
23
24
25
26
27
28
29
30
Servicing
Standard Practices & EZAP
Air Conditioning
Auto Flight
Communications
Electrical Power
Equipment & Furnishings
Fire Protection
Flight Controls
Fuel
Hydraulic Power
Ice & Rain Protection
31
32
33
34
35
36
38
49
51
52
53
54
55
Indicating & Recording System
Landing Gear
Lights
Navigation
Oxygen
Pneumatic
Water & Waste
Airborne Auxiliary Power Unit (APU)
Standard Practices & Structures
Doors (Mechanical)
Fuselage Drains
Nacelles/Pylons
Stabilizers
56
57
70
71
72
73
74
75
76
77
78
79
80
Windows
Wings
Standard Practices - Engine
Powerplant
Engine
Engine Fuel & Control
Ignition
Air
Engine Controls
Engine Indicating
Exhaust
Oil
Starting
Rev 0 19 March 2014
2-2
MD-80 MAINTENANCE MANUAL
2.4 Systems and Powerplant Program
1. Service Check / Pre-flight Inspection.
A service check / pre-flight inspection will be accomplished prior to the first flight of the day and will also be accomplished in conjunction with any higher level inspection.
A service check / pre-flight inspection consists of a walk around inspection of specific items and correction of maintenance log book items.
2. Electrical Wiring Interconnection Systems (EWIS) maintenance program.
The EWIS maintenance program is based on EWIS Instructions for Continued Airworthiness (ICA) and published in the MD-80 Maintenance Implementation Document (MID) (ME80-016). These items are included in this maintenance program.
All EWIS tasks have been identified by adding the notation (EZAP) to the task description.
Those EWIS items added by Supplemental Type Certificate (STC) (STC ST02434LA) will have inspec-tions located in the ICA section of that STC and that have been approved by the FAA Oversight Office, and as such not covered in this program.
3. Fuel Tank System (SFAR 88) Maintenance Program.
The fuel tank system inspection program was based on fuel tank system Instructions for Continued Air-worthiness (ICA) and published in the MD-80 Maintenance Implementation Document (MID) (ME80-016) section 3 and the DC-9 / MD-80 / MD-90 / 717 Special Compliance Item (MDC-92K9145). They have been developed in accordance with the applicable provisions of SFAR 88. These items are included in this maintenance program, this meets the requirements set forth in Title 14 CFR 125.507.
Those items effected by Supplemental Type Certificate (STC) (STC ST02434LA) will have inspections located in the ICA section of that STC and that have been approved by the FAA Oversight Office, and as such not covered in this program.
2.4.1 DFDR Maintenance Program (14 CFR Part 121.344(a)(b)(c))
2.4.1.1 General
Everts Air Cargo has selected the Solid State Digital Flight Data Recorder (SSDFDR) Fairchild Model FA2100FDR for installation on its DC-9-80 series aircraft. All maintenance operation on this recorder sys-tem will be accomplished as outlined in the STC ST01554AT document, Boeing MRB ME-MRB-80 docu-ment, and Boeing Aircraft Maintenance Manual TP-80MM-TNK.
2.4.1.2 System Description
The Fairchild SSDFDR meets or exceeds the requirements of Federal Aviation Administration (FAA) Technical Standard Order TSO-C124a, and is classified as a Class A Flight Data Recorder IAW EURO-CAE MOPS ED-55. The recorder is capable of storing a minimum of 25 hours of flight data that can be downloaded in less than 4 minutes. For more details please reference STC ST01554AT and Boeing Aircraft Maintenance Manual TP-80MM-TNK.
Rev 0 19 March 2014
2-3
MD-80 MAINTENANCE MANUAL
2.4.1.3 Scheduled Maintenance Tasks
All scheduled maintenance tasks will be accomplished as required by the Boeing Maintenance Review Board Report ME-MRB-80 and tracked by task card. The EAC maintenance program contains the follow-ing task cards in support of DFDR maintenance:
The CAS reporting system described in the Everts Air Cargo GMM will be used to determine the effective-ness of this maintenance program and may be adjusted as required to meet the reliability standard deter-mined by CAS Board Members.
2.4.1.4 Data Conversion SSDFDR
Data is recorded using the FA2100 SSDFDR. Every 1C inspection this data is downloaded using a inter-face unit and sent to an independent company for analysis. A converted document is sent back to EAC for review. If there are any anomalies, the necessary maintenance actions will be taken. All downloaded data will be stored in the Inspection department.
2.4.1.5 Functional Checks
The Model FA2100 FDR does not require scheduled maintenance or calibration, except for periodic inspection and servicing of the Underwater Locator Device. Unscheduled maintenance and functional checks will be accomplished per Boeing Aircraft Maintenance Manual TP-80MM-TNK 31-31-00.
2.4.1.6 Underwater Locator Device (ULD)
The Model FA2100 FDR is equipped with an ULD that is approved to FAA TSO-C121 and exceeds requirements of HBAW 92-07, Maintenance of Acoustic Underwater Locator Beacons, and FAA order 8300.10 Volume 3, chapter 142. The ULD is mounted horizontally on the front of the CSMU for easy removal and viewing of the battery expiration date. Maintenance of the ULD will be performed per Boeing MD-80 Aircraft Maintenance Manual TP-80MM-TNK 31-31-12.
2.4.1.7 Correlation Requirements
Correlation requirements of the inputs to the SSDFDR will perform as stated in the Boeing MRB ME-MRB-80 and may be adjusted as required to meet the reliability standard determined by the CAS Board.
2.4.1.8 Accessing Online References
The following instruction will assist you in navigating around the L-3 website.1. Open your web browser and type into the address bar: www.l-3ar.net
2. Select “enter”. At the top of the page will be a link for “Aviation Recorders”. Click on this link.3. A login page will come up next. Enter, in lower case, the user name (evertsair) and password
(dumbo). Click on the “I Accept” box and select “Log In”.4. You will be directed to a list of publications segregated by model number. Publications for our
DFDR model are found under:
“Model FA2100 Solid State Flight Data Recorder Publications (ATA 31-30-03)”5. Click on “All Technical Manuals – CMM’s and I/O’s”. Component Maintenance Manuals and
Installations and Operation Manuals are now available to the user.
NOTE: You must have Adobe Acrobat in order to view the manuals since they are stored as PDF files.
The Component Maintenance Manual is used to perform shop level maintenance.
Task Description Interval31-031-01 Functional check of all required Parameters Being
Recorded properly by the Flight Recorder NOTE: Recording of parameters and tolerances specified by Title 14 CFR, Part 121 Appx. B must be verified
1C inspection
31-031-02 Replace DFDR Underwater LocatorBattery and Ops Check Underwater Locator Beacon
6 years
Rev 0 19 March 2014
2-4
MD-80 MAINTENANCE MANUAL
2.5 Notes: ATA 49 (APU)
1. Off-aircraft tasks not specified herein shall be controlled by Everts based on OEM approved manuals.
2. Identification of life-limited parts controlled by the APU manufacturer is provided in the APU Engine Inspection/Repair Manual.
3. The tasks listed are to be accomplished at the specified intervals. The most appropriate task interval has been used in determining the APU scheduled maintenance task requirements. Operators may develop conversion factors (i.e., APU cycles to flight hours) with the approval of their regulating authorities for incorporation into their own scheduled maintenance program, provided such conversion does not exceed the interval shown for the tasks.
4. Mandatory threshold inspections are not required for the auxiliary power unit. The manufacturer may recommend such inspections in the event that late development or in-service experience would dictate the need to examine specific components of the APU. If this is necessary, direct negotiations between applicable operators and the APU manufacturer will be necessary. Results of these inspections should be made available by the APU manufacturer to other customer airlines as well as the regulatory author-ities.
5. Opportunity inspections may be used for sampling certain components and accessories defined by the APU manufacturer’s approved maintenance manual and/or service bulletin. Opportunity inspections for other APU components or accessories may be recommended, and if required, the operators will be requested by the APU manufacturer to cooperate in obtaining necessary samples on an “as required” basis. Results of these inspections should be made available by the APU manufacturer to other cus-tomer airlines as well as the regulatory authorities.
2.6 Notes: ATA 71-80 (Powerplant)
1. With the exception of life-limited parts, off-wing (in-shop) maintenance tasks are not included herein. Off-wing tasks shall be controlled by Everts based on their specific maintenance programs and approved manuals.
2. Limitations of life-limited parts are controlled by the engine manufacturers and are published in the Engine Manuals, Section 5. The declared life of these life-limited parts will be lower than the ultimate Predicted Safe Cycle Life (PSCL). A life sampling program to justify an extension to the declared life up to the PSCL in increments will be an approved method of achieving life extensions.
3. There are no mandatory Threshold Inspections required. Engine manufacturers may recommend such inspections in the event that in-service experience would dictate the need to examine specific compo-nents of individual engines. If this is required, direct negotiations between applicable operators and the engine manufacturers will be necessary. Results of these inspections should be made available by the engine manufacturers to other customer airlines as well as the regulatory authorities.
4. Opportunity Inspections of certain engine components and accessories may be recommended. No spe-cific list of items will be included; however, if the need exists, operators will be requested by the engine manufacturers to cooperate in obtaining necessary samples on an “as required” basis. Results of these inspections should be made available by the engine manufacturers to other customer airlines as well as the regulatory authorities.
Rev 0 19 March 2014
2-5
MD-80 MAINTENANCE MANUAL
Figure 2-A: Systems and Powerplant Maintenance Program Example Page
Rev 0 19 March 2014
2-6
MD-80 MAINTENANCE MANUAL
2.7 Page Format Explanation
1. MPD Item Number
Each task is given a unique MPD item number. The first and second digit is the ATA number. The rest of the numbers denote the MPD sequence number.
When a maintenance task is added by Everts and not part of the Boeing MD-80 MPD it will be identified by the three letter code TNK in the middle 3 digits of the task number. These Tasks will be inserted into Appx A of this manual until the next Boeing revision cycle when they can be entered into the Boeing task card manual at which time they will be removed from Appx A. The Chief Inspector and Director of Main-tenance have control of addition and removal of content of Appx A and the LEP will be signed by one of them with the current date.
2. AMM Reference
Airplane Maintenance Manual procedure (Chapter, Section, Subject) which supports the MPD require-ment.
3. CAT Failure-Effect Categories (CAT) and Regulatory Requirements
All tasks listed in this section have a “category” identification as follows:
• 5 - Evident, Safety.
• 6 - Evident, Economic (Operational).
• 7 - Evident, Economic (Non-Operational).
• 8 - Hidden, Safety.
• 9 - Hidden, Non-Safety.
• _ - A blank indicates this task is a non-MRB item.
4. Task MSG-3 Task Categories
LUB = LUBRICATION - Consumable replenishment by lubricating.
SVC = SERVICING - Consumable replenishment by servicing.
OPC = OPERATIONAL CHECK - A failure finding task to determine if an item is fulfilling its intended purposes. Does not require quantitative tolerances.
VCK = VISUAL CHECK - A visual failure finding task through observation to determine if an item is fulfilling its intended purpose. Does not require quantitative tolerances.
GVI = INSPECTION - GENERAL VISUAL - A visual examination that will detect obvious unsatis-factory conditions.
FNC = FUNCTIONAL CHECK - A quantitative check to determine if one or more functions of an item performs within specified limits. This is a potential failure finding task.
DET = INSPECTION - DETAILED - An intensive visual examination of a specified detail, assembly, or installation. A potential failure finding task.
RST = RESTORATION - Reworking, replacement of parts or cleaning necessary to return an item to a specific standard.
DIS = DISCARD - The removal from service of an item at a specified life limit.
SDI = SPECIAL DETAILED INSPECTION - Similar to Detailed Inspection but requires some special inspection technique such as non-destructive inspection, dye penetrant, high powered magnification, etc.
5. Interval
Task intervals are specified in terms of letter checks. Some tasks are specified in terms of usage parameters such as flight hours, flight cycles, or calender time.
Rev 0 19 March 2014
2-7
MD-80 MAINTENANCE MANUAL
DY = Days.
FC = Airplane Flight Cycles.
APU CNG = APU Change.
FH = Airplane Flight Hours.
AHR = APU Hours.
YRS = Years.
ENG CNG = Engine Change.
LDG CNG = Landing Gear Change.
LIF LIM = Life Limited.
NAT REQ = Regulatory Authority Requirement.
TRANSIT = Transit.
NOTE = Interval note.
6. Access and Zone
The Zone identifies where the task is performed on the airplane. Access Data and Zones are defined in Appendix A, “Access Data and Zone Diagrams.”
7. Applicability
Airplane (APL) Model:
• ALL = All MD-80 Airplanes.
• MD-81.
• MD-82.
• MD-83.
• MD-87.
• MD-88.
Engine (ENG):
• ALL = All Engines.
8. Labor-Hours
Estimated Labor-hours (per airplane) required to perform the task(s). These labor-hours do not include the time required to gain access, position work stands, defuel and purge fuel tanks, troubleshoot, nor correct discrepancies found while performing the task. The labor-hours estimates are based on the use of skilled personnel and ready availability of required tools and equipment.
9. Task Description
Description of the task to be performed. Airplane notes and Interval notes are listed following the task description to provide additional explanation of interval and airplane configuration.
Rev 0 19 March 2014
2-8
MD-80 MAINTENANCE MANUAL
BO
EIN
G P
RO
PR
IETA
RY
- C
opyr
ight
© U
npub
lishe
d W
ork
- See
title
pag
e fo
r det
ails
AU
GU
ST
2013
ME
80-0
20-T
NK
PA
GE
1.1
-1
0 1 2 3 4 5 7A
TA 0
5: T
IME
LIM
ITS/
MA
INTE
NA
NC
E C
HEC
KS
U8
05-0
01-0
105
-00-
00-2
10V
CK
DA
ILY
DA
ILY
10 20 30 40 44 50 58 60 70
0.75
Per
form
dai
ly w
alk
arou
nd o
f airc
raft.
AIR
PLA
NE
NO
TE: A
ll E
TOP
S it
ems
mus
t be
acco
mpl
ishe
d an
d si
gned
by
ETO
PS
qua
lifie
d pe
rson
nel n
o le
ss th
an th
ree
hour
s pr
ior t
o de
partu
re.
ETO
PS
item
s ar
e ap
plic
able
to A
LL a
ircra
ft (E
TOP
S a
nd N
ON
ETO
PS
) exc
ept
as n
oted
"ETO
PS
ON
LY).
U9
05-0
01-0
205
-00-
00-2
10V
CK
3 D
Y3
DY
10 17 18 55 56 81 82
2.50
Do
a se
rvic
e ch
eck
of th
e ai
rcra
ft.
AIR
PLA
NE
NO
TE: E
TOP
S it
ems
are
appl
icab
le to
ALL
airc
raft
(ETO
PS
and
N
ON
ETO
PS
) exc
ept a
s no
ted
"ETO
PS
ON
LY).
All
ETO
PS
item
mus
t be
acco
mpl
ishe
d an
d si
gned
by
ETO
PS
qua
lifie
d pe
rson
nel n
o le
ss th
an th
ree
hour
s pr
ior t
o an
ETO
PS
dep
artu
re.
10A
TA 2
0: S
TAN
DA
RD
PR
AC
TIC
ES -
AIR
FRA
ME
U11
20-0
10-0
120
-51-
01-1
60R
ST
4 C
4 C
4545
01A
NO
TE0.
33C
lean
are
a of
dus
t, lin
t and
all
fore
ign
obje
cts
- E a
nd E
Com
partm
ent (
EZA
P).
AC
CE
SS
NO
TE: D
o no
t dis
turb
any
sys
tem
s in
stal
latio
ns
U12
20-0
10-0
220
-51-
01-1
60R
ST
4 C
4 C
51N
OTE
0.33
Cle
an a
rea
of d
ust,
lint a
nd a
ll fo
reig
n ob
ject
s - F
orw
ard
Car
go C
ompa
rtmen
t U
pper
Tun
nels
and
Und
er S
ide
of C
abin
Ven
ts (C
usp
Hol
es) (
EZA
P).
AC
CE
SS
NO
TE: O
pen
acce
ss p
anel
s as
requ
ired.
Do
not d
istu
rb a
ny s
yste
ms
inst
alla
tions
.
U13
20-0
10-0
320
-51-
01-1
60R
ST
4 C
4 C
53N
OTE
0.33
Cle
an a
rea
of d
ust,
lint a
nd a
ll fo
reig
n ob
ject
s - A
rea
betw
een
Low
er S
urfa
ce o
f C
abin
Flo
or to
Upp
er S
urfa
ce o
f Cen
ter W
ing
Cen
ter W
ing
(EZA
P).
AC
CE
SS
NO
TE: O
pen
acce
ss p
anel
s as
requ
ired.
Do
not d
istu
rb a
ny s
yste
ms
inst
alla
tions
.
U14
20-0
10-0
420
-50-
00-2
10G
VI
4 C
4 C
53N
OTE
0.33
Gen
eral
Vis
ual I
nspe
ctio
n of
Vap
or B
arrie
r - A
rea
betw
een
Low
er S
urfa
ce o
f C
abin
Flo
or to
Upp
er S
urfa
ce o
f Cen
ter W
ing
(EZA
P).
AC
CE
SS
NO
TE: O
pen
acce
ss p
anel
s as
requ
ired.
Do
not d
istu
rb a
ny s
yste
ms
inst
alla
tions
.
DC
-9-8
0SF
Mai
nten
ance
Pla
nnin
g D
ocum
ent
SYST
EMS
AN
D P
OW
ERPL
AN
T M
AIN
TEN
AN
CE
PRO
GR
AM
MPD
ITEM
NU
MB
ERAM
M
REF
EREN
CE
C A T
T A S K
INTE
RVA
L
THR
ES.
REP
EAT
TASK
DES
CR
IPTI
ON
ZON
EAC
CES
SM
AN-
HO
UR
S
Rev 0 19 March 2014
2-9
MD-80 MAINTENANCE MANUAL
BO
EIN
G P
RO
PR
IETA
RY
- C
opyr
ight
© U
npub
lishe
d W
ork
- See
title
pag
e fo
r det
ails
AU
GU
ST
2013
ME
80-0
20-T
NK
PA
GE
1.1
-2
0 1 2 3 4 5
DC
-9-8
0SF
Mai
nten
ance
Pla
nnin
g D
ocum
ent
SYST
EMS
AN
D P
OW
ERPL
AN
T M
AIN
TEN
AN
CE
PRO
GR
AM
MPD
ITEM
NU
MB
ERAM
M
REF
EREN
CE
C A T
T A S K
INTE
RVA
L
THR
ES.
REP
EAT
TASK
DES
CR
IPTI
ON
ZON
EAC
CES
SM
AN-
HO
UR
S
U15
20-0
10-0
520
-51-
01-1
60R
ST
2 C
2 C
57N
OTE
0.33
Cle
an a
rea
of d
ust,
lint a
nd a
ll fo
reig
n ob
ject
s - A
ft C
argo
Com
partm
ent (
EZA
P).
AC
CE
SS
NO
TE: O
pen
acce
ss p
anel
s as
requ
ired.
Do
not d
istu
rb a
ny s
yste
ms
inst
alla
tions
.
U16
20-0
10-0
620
-51-
01-1
60R
ST
4 C
4 C
57N
OTE
0.33
Cle
an a
rea
of d
ust,
lint a
nd a
ll fo
reig
n ob
ject
s - A
ft C
argo
Com
partm
ent,
Upp
er
Tunn
els
and
Und
er S
ide
of C
abin
Ven
ts (C
usp
Hol
es) (
EZA
P).
AC
CE
SS
NO
TE: O
pen
acce
ss p
anel
s as
requ
ired.
Ref
er to
AM
M C
hapt
er 0
6 fo
r pr
oper
acc
ess
pane
l num
ber.
Do
not d
istu
rb a
ny s
yste
ms
inst
alla
tions
.
U17
20-0
10-0
720
-50-
00-2
10G
VI4
C4
C45
4501
A0.
60In
spec
t (G
VI) a
ll EW
IS in
the
zone
incl
udin
g th
e ai
rcra
ft ba
tterie
s E
WIS
in E
&E
co
mpa
rtmen
t. (E
ZAP
)
U18
20-0
10-0
820
-50-
00-2
10G
VI
4 C
4 C
43N
OTE
0.60
Insp
ect (
GV
I) al
l EW
IS in
the
nose
gea
r whe
el w
ell a
nd u
npre
ssur
ized
sid
ewel
ls.
(EZA
P)
AC
CE
SS
NO
TE: G
ear d
oors
ope
n.
U19
20-0
10-0
920
-50-
00-2
10G
VI
4 C
4 C
51N
OTE
0.60
Insp
ect (
GV
I) al
l EW
IS in
the
forw
ard
carg
o co
mpa
rtmen
t. (E
ZAP
)
AC
CE
SS
NO
TE: C
eilin
g an
d si
dew
all p
anel
s re
mov
ed.
U20
20-0
10-1
020
-50-
00-2
10G
VI
8 C
8 C
2323
01C
2302
CN
OTE
0.60
Insp
ect (
GV
I) of
all
expo
sed
EW
IS in
the
cent
er w
ing
sect
ion.
(EZA
P)
AC
CE
SS
NO
TE: R
ear p
anel
s re
mov
ed.
U21
20-0
10-1
120
-50-
00-2
10G
VI
2 C
2 C
55 56N
OTE
0.60
Insp
ect (
GV
I) al
l exp
osed
EW
IS in
the
mai
n la
ndin
g ge
ar w
heel
wel
ls. (
EZA
P)
AC
CE
SS
NO
TE: G
ear d
oors
ope
n.
U22
20-0
10-1
220
-50-
00-2
10G
VI
4 C
4 C
57N
OTE
0.60
Insp
ectio
n (G
VI)
all E
WIS
in th
e af
t car
go c
ompa
rtmen
t. (E
ZAP
)
AC
CE
SS
NO
TE: R
emov
e al
l cei
ling
and
side
wal
l pan
els.
U23
20-0
10-1
320
-50-
00-2
11D
ET
4 C
4 C
43 44 45 46 51 53 57 58 59
4501
AN
OTE
2.00
Det
aile
d in
spec
tion
of th
e el
ectri
cal m
ain
feed
er c
able
s an
d al
l exp
osed
EW
IS
(EZA
P).
AC
CE
SS
NO
TE: R
emov
e le
ft si
de o
utbo
ard
pass
enge
r sea
ts, l
eft s
ide
outb
oard
flo
or p
anel
s in
the
pass
enge
r cab
in, a
nd fo
rwar
d, m
id, a
nd a
ft ca
rgo
com
partm
ent l
eft s
ide
uppe
r sid
ewal
l pan
els.
Rev 0 19 March 2014
2-10
MD-80 MAINTENANCE MANUAL
BO
EIN
G P
RO
PR
IETA
RY
- C
opyr
ight
© U
npub
lishe
d W
ork
- See
title
pag
e fo
r det
ails
AU
GU
ST
2013
ME
80-0
20-T
NK
PA
GE
1.1
-3
0 1 2 3 4 5
DC
-9-8
0SF
Mai
nten
ance
Pla
nnin
g D
ocum
ent
SYST
EMS
AN
D P
OW
ERPL
AN
T M
AIN
TEN
AN
CE
PRO
GR
AM
MPD
ITEM
NU
MB
ERAM
M
REF
EREN
CE
C A T
T A S K
INTE
RVA
L
THR
ES.
REP
EAT
TASK
DES
CR
IPTI
ON
ZON
EAC
CES
SM
AN-
HO
UR
S
U24
20-0
10-1
420
-51-
01-1
60R
ST
4 C
4 C
4243
02A
NO
TE0.
33C
lean
are
a of
dus
t, lin
t and
all
fore
ign
obje
cts
- For
war
d A
cces
sory
C
ompa
rtmen
t (E
ZAP
).
AC
CE
SS
NO
TE: D
o no
t dis
turb
any
sys
tem
s in
stal
latio
ns.
U25
20-0
20-0
120
-51-
01-1
60R
ST
4 C
4 C
44N
OTE
0.33
Cle
an a
rea
of d
ust,
lint a
nd a
ll fo
reig
n ob
ject
s - C
ockp
it A
rea,
Low
er S
idew
alls
, Fl
oor A
rea
and
Fron
t Sid
e of
EP
C (E
ZAP
).
AC
CE
SS
NO
TE: O
pen
acce
ss p
anel
s as
requ
ired.
Do
not d
istu
rb a
ny s
yste
ms
inst
alla
tions
.
U26
20-0
20-0
220
-51-
01-1
60R
ST
8 C
8 C
4646
01A
4603
AN
OTE
0.33
Cle
an a
rea
of d
ust,
lint a
nd a
ll fo
reig
n ob
ject
s - E
PC
, Aft
Sid
e (E
ZAP
).
AC
CE
SS
NO
TE: O
pen
acce
ss p
anel
s as
requ
ired.
Do
not d
istu
rb a
ny s
yste
ms
inst
alla
tions
.
U27
20-0
20-0
420
-50-
00-2
10G
VI
4 C
4 C
44N
OTE
0.60
Insp
ect (
GV
I) al
l exp
osed
EW
IS in
coc
kpit
area
. (E
ZAP
)
AC
CE
SS
NO
TE: O
pen
all p
anel
s, in
clud
ing
floor
, EP
C a
nd a
cces
sibl
e ar
ea
behi
nd In
stru
men
t pan
el. I
nstru
men
t rem
oval
not
requ
ired.
U28
20-0
30-0
120
-51-
01-2
11D
ET
1 C
1 C
59N
OTE
0.67
Det
aile
d In
spec
tion
of a
ll ex
pose
d E
WIS
in th
e ar
ea o
f the
Ble
ed A
ir D
uct J
oint
s (A
ft si
de o
f Aft
Pre
ssur
e B
ulkh
ead,
Lef
t and
Rig
ht S
ide)
(EZA
P).
AC
CE
SS
NO
TE: O
pen
acce
ss p
anel
s as
requ
ired.
Do
not d
istu
rb a
ny s
yste
ms
inst
alla
tions
.
U29
20-0
30-0
220
-50-
00-2
10G
VI
2 C
2 C
5959
03A
5904
A0.
60In
spec
t (G
VI)
the
all e
xpos
ed E
WIS
in th
e A
PU
com
partm
ent.
(EZA
P)
U30
20-0
40-0
120
-50-
00-2
10G
VI
1 A
1 A
71 72 77 78
NO
TE0.
60In
spec
t ( G
VI)
the
all e
xpos
ed E
WIS
in th
e le
ft an
d rig
ht p
ower
plan
ts a
nd c
owl
hing
ed d
oors
. (E
ZAP
)
AC
CE
SS
NO
TE: O
pen
Cow
lings
.
U31
20-0
50-0
120
-50-
00-2
10G
VI
8 C
8 C
13N
OTE
0.60
Insp
ect (
GV
I) al
l exp
osed
EW
IS in
the
left
win
g in
ters
par b
ox s
ectio
n. (E
ZAP
)
AC
CE
SS
NO
TE: A
ll pa
nels
rem
oved
U32
20-0
50-0
220
-50-
00-2
10G
VI
4 C
4 C
15N
OTE
0.60
Insp
ect (
GV
I) le
ft w
ing
all e
xpos
ed E
WIS
from
rear
spa
r to
trailin
g ed
ge. (
EZA
P)
AC
CE
SS
NO
TE: F
laps
low
ered
, spo
ilers
rais
ed a
nd a
ll hi
nged
pan
els
low
ered
.
Rev 0 19 March 2014
2-11
MD-80 MAINTENANCE MANUAL
BO
EIN
G P
RO
PR
IETA
RY
- C
opyr
ight
© U
npub
lishe
d W
ork
- See
title
pag
e fo
r det
ails
AU
GU
ST
2013
ME
80-0
20-T
NK
PA
GE
1.1
-4
0 1 2 3 4 5
DC
-9-8
0SF
Mai
nten
ance
Pla
nnin
g D
ocum
ent
SYST
EMS
AN
D P
OW
ERPL
AN
T M
AIN
TEN
AN
CE
PRO
GR
AM
MPD
ITEM
NU
MB
ERAM
M
REF
EREN
CE
C A T
T A S K
INTE
RVA
L
THR
ES.
REP
EAT
TASK
DES
CR
IPTI
ON
ZON
EAC
CES
SM
AN-
HO
UR
S
U33
20-0
60-0
120
-50-
00-2
10G
VI
8 C
8 C
1414
54C
1456
C14
60C
1462
C14
64C
1466
C14
70C
1472
C14
76C
1478
C
0.60
Insp
ect (
GV
I) al
l exp
osed
EW
IS in
the
right
win
g in
ters
par b
ox s
ectio
n. (E
ZAP
)
U34
20-0
60-0
220
-50-
00-2
10G
VI
4 C
4 C
16N
OTE
0.60
Insp
ect (
GV
I) rig
ht w
ing
all e
xpos
ed E
WIS
from
rear
spa
r to
trailin
g ed
ge.
(EZA
P)
AC
CE
SS
NO
TE: F
laps
low
ered
, spo
ilers
rais
ed a
nd a
ll hi
nged
pan
els
low
ered
35A
TA 2
1: A
IR C
ON
DIT
ION
ING
U36
21-0
01-0
021
-20-
02-1
60R
ST
24 M
O24
MO
591.
00C
lean
the
Air
Con
ditio
ning
Wat
er S
epar
ator
Dra
in L
ines
U37
21-0
21-0
121
-52-
04-2
117
DE
T4
C4
C45
0.03
Det
aile
d In
spec
tion
of th
e Le
ft an
d R
ight
Che
ck V
alve
s Fl
appe
r and
Hin
ge P
ins
(Avi
onic
s C
ompt
Ven
turi/
Rad
io R
ack
Coo
ling)
U38
21-0
21-0
221
-52-
02-7
109
OP
C4
C4
C44 45
0.03
Ope
ratio
nal c
heck
of t
he ra
dio
rack
coo
ling
syst
em v
entu
ri m
ode.
U39
21-0
22-0
121
-20-
01-2
1121
-20-
09-2
1121
-20-
13-2
11
6 7 9
DE
T4
C4
C58 59
0.33
Det
aile
d In
spec
tion
of th
e C
old
Air,
Con
ditio
ned
Air,
Rec
ircul
atio
n Fa
n, G
roun
d C
ondi
tione
d A
ir an
d G
roun
d A
ir C
onne
ctor
Che
ck V
alve
s Fl
appe
r and
Hin
ge
Pin
s
U40
21-0
22-0
221
-20-
19-9
026
RS
T1
C1
C46 58
0.67
Cle
an th
e C
abin
Air
Exh
aust
Baf
fles
U41
21-0
22-0
321
-20-
18-9
017
DIS
1 C
1 C
5757
03C
0.08
Dis
card
the
Rec
ircul
atio
n Fa
n Fi
lters
U42
21-0
22-0
406
-24-
00-2
119
DE
T4
C4
C57
5906
C0.
03D
etai
led
Insp
ectio
n of
the
Gro
und
Con
ditio
ned
Air
Acc
ess
Doo
r Hin
ge a
nd L
atch
A
ssem
bly
U43
21-0
26-0
121
-50-
01-7
109
OP
C2
C2
C44
0.08
Ope
ratio
nal C
heck
of t
he C
oolin
g Fa
n D
iver
ter a
nd M
anifo
ld C
heck
Val
ves
U44
21-0
29-0
121
-20-
07-7
109
OP
C2
C2
C44 59
0.02
Ope
ratio
nal C
heck
of t
he R
am A
ir V
alve
Sys
tem
U45
21-0
31-0
112
-21-
03-6
406
LUB
1 C
1 C
5757
36C
5738
C0.
02Lu
bric
ate
the
Out
flow
Val
ve a
nd B
utte
rfly
Val
ve A
ssem
blie
s
U46
21-0
31-0
221
-32-
05-2
116
DE
T4
C4
C57
5736
C57
38C
0.03
Det
aile
d In
spec
tion
of th
e O
utflo
w V
alve
and
But
terfl
y V
alve
Ass
embl
ies
U47
21-0
31-0
321
-32-
05-6
156
RS
T1
C1
C57
5736
C57
38C
0.03
Cle
an th
e O
utflo
w V
alve
and
But
terfl
y V
alve
Ass
embl
ies
Rev 0 19 March 2014
2-12
MD-80 MAINTENANCE MANUAL
BO
EIN
G P
RO
PR
IETA
RY
- C
opyr
ight
© U
npub
lishe
d W
ork
- See
title
pag
e fo
r det
ails
AU
GU
ST
2013
ME
80-0
20-T
NK
PA
GE
1.1
-5
0 1 2 3 4 5
DC
-9-8
0SF
Mai
nten
ance
Pla
nnin
g D
ocum
ent
SYST
EMS
AN
D P
OW
ERPL
AN
T M
AIN
TEN
AN
CE
PRO
GR
AM
MPD
ITEM
NU
MB
ERAM
M
REF
EREN
CE
C A T
T A S K
INTE
RVA
L
THR
ES.
REP
EAT
TASK
DES
CR
IPTI
ON
ZON
EAC
CES
SM
AN-
HO
UR
S
U48
21-0
31-0
421
-32-
00-7
109
OP
C4
C4
C57
5736
C57
38C
0.01
Ope
ratio
nal C
heck
of t
he O
utflo
w V
alve
Man
ual C
ontro
l Sys
tem
U49
21-0
31-0
521
-32-
05-7
209
FNC
4 C
4 C
5757
36C
5738
C0.
22Fu
nctio
nal C
heck
of t
he O
utflo
w V
alve
Man
ual C
ontro
l Cab
le S
yste
m
U50
21-0
31-0
621
-32-
00-2
119
DE
T4
C4
C45 51 57
0.66
Det
aile
d In
spec
tion
of th
e O
utflo
w V
alve
Man
ual C
ontro
l Cab
les
U51
21-0
32-0
521
-32-
05-9
02R
ST
1500
0 FH
NO
TE15
000
FHN
OTE
575.
00R
esto
ratio
n of
the
Cab
in A
ir O
utflo
w V
alve
Act
uato
r
AIR
PLA
NE
NO
TE: T
his
task
car
d pe
rtain
s to
Hon
eyw
ell C
abin
Pre
ssur
e C
ontro
ller (
P/N
211
8490
-4).
INTE
RV
AL
NO
TE: A
pplic
able
to C
abin
Pre
ssur
e C
ontro
ller (
CP
C),
part
num
ber
(P/N
) 211
8490
-4.
Ref
er to
MD
-80-
SL-
21-1
02.
U52
21-0
33-0
121
-32-
06-7
208 9
FNC
2 C
2 C
44 5858
05C
0.26
Func
tiona
l Che
ck o
f the
Cab
in L
ow P
ress
ure
War
ning
and
Indi
catio
n S
yste
m
U53
21-0
34-0
121
-32-
07-7
208 9
FNC
4 C
4 C
51N
OTE
0.05
Func
tiona
l Che
ck o
f the
Cab
in P
ositi
ve P
ress
ure
Rel
ief V
alve
s
AC
CE
SS
NO
TE: R
efer
to C
hapt
er 0
6 of
you
r AM
M fo
r pro
per p
anel
num
ber.
U54
21-0
34-0
221
-32-
08-7
109
OP
C4
C4
C51 57
5151
C51
63C
5722
C
0.01
Ope
ratio
nal C
heck
of t
he C
abin
Equ
aliz
atio
n V
alve
s
U55
21-0
34-0
321
-00-
00-7
109
OP
C4
C4
C57
5703
C0.
08O
pera
tiona
l Che
ck o
f the
Neg
ativ
e P
ress
ure
Rel
ief V
alve
U56
21-0
34-0
421
-00-
00-2
119
DE
T4
C4
C57
5703
C0.
08D
etai
led
Insp
ectio
n of
the
Neg
ativ
e P
ress
ure
Rel
ief V
alve
U57
21-0
34-0
521
-32-
07-9
029
RS
T4
C4
C51
NO
TE0.
03C
lean
the
Pos
itive
Pre
ssur
e R
elie
f Val
ve F
ilter
AC
CE
SS
NO
TE: R
efer
to C
hapt
er 0
6 of
you
r AM
M fo
r pro
per p
anel
num
ber.
U58
21-0
53-0
112
-12-
03-6
126
SV
C2
A2
A59
0.13
Ser
vice
the
Air
Cyc
le M
achi
ne (A
CM
)
U59
21-0
53-0
221
-51-
02-9
0221
-51-
03-9
0221
-51-
04-9
0221
-51-
05-9
02
6R
ST
2 C
2 C
5961
01A
0.66
Cle
an th
e P
rimar
y an
d S
econ
dary
Hea
t Exc
hang
ers
U60
21-0
53-0
321
-61-
04-7
209
FNC
2 C
2 C
4545
01A
0.20
Func
tiona
l Che
ck o
f the
Sup
ply
Tem
pera
ture
Hig
h S
yste
m S
enso
r and
Ale
rts
U61
21-0
54-0
121
-20-
02-9
026
RS
T1
C1
C59
6101
A0.
33C
lean
the
Coa
lesc
er B
ag
U62
21-0
55-0
221
-20-
06-9
029
RS
T2
C2
C59
5910
A0.
08C
lean
the
Ram
Air
Coo
ling
Fan
Pro
tect
ion
Scr
een
U63
21-0
55-0
321
-20-
05-2
119
DE
T4
C4
C59
5910
A0.
16D
etai
led
Insp
ectio
n of
the
Div
erte
r Val
ves
Flap
per a
nd H
inge
Pin
s
Rev 0 19 March 2014
2-13
MD-80 MAINTENANCE MANUAL
BO
EIN
G P
RO
PR
IETA
RY
- C
opyr
ight
© U
npub
lishe
d W
ork
- See
title
pag
e fo
r det
ails
AU
GU
ST
2013
ME
80-0
20-T
NK
PA
GE
1.1
-6
0 1 2 3 4 5
DC
-9-8
0SF
Mai
nten
ance
Pla
nnin
g D
ocum
ent
SYST
EMS
AN
D P
OW
ERPL
AN
T M
AIN
TEN
AN
CE
PRO
GR
AM
MPD
ITEM
NU
MB
ERAM
M
REF
EREN
CE
C A T
T A S K
INTE
RVA
L
THR
ES.
REP
EAT
TASK
DES
CR
IPTI
ON
ZON
EAC
CES
SM
AN-
HO
UR
S
U64
21-0
56-0
321
-31-
04-7
209
FNC
2 C
2 C
580.
06Fu
nctio
nal C
heck
of t
he A
uto
Pac
k S
hutd
own
Con
ditio
n A
ir Th
erm
al S
witc
h
U65
21-0
56-0
421
-31-
05-7
209
FNC
2 C
2 C
5959
10A
0.08
Func
tiona
l Che
ck o
f the
Aut
o P
ack
Shu
tdow
n Tu
rbin
e In
let T
herm
al S
witc
h
U66
21-0
56-0
521
-31-
05-7
209
FNC
2 C
2 C
5959
10A
0.08
Func
tiona
l Che
ck o
f the
Com
pres
sor D
isch
arge
The
rmal
Sw
itch
U67
21-0
62-0
121
-61-
02-1
106 7
RS
T2
C2
C58
5823
C0.
25C
lean
the
Cab
in A
ir Te
mpe
ratu
re S
enso
r and
Air
Sen
sor E
ject
or
U68
21-0
62-0
221
-61-
05-7
206 9
FNC
2 C
2 C
580.
25Fu
nctio
nal C
heck
of t
he C
ockp
it S
uppl
y Te
mpe
ratu
re H
igh
Sys
tem
and
Ale
rts
69A
TA 2
2: A
UTO
FLI
GH
T
U70
22-0
01-0
022
-01-
05-7
41O
PC
450
FH45
0 FH
440.
50R
etur
n-to
-Ser
vice
(RTS
) Che
ck o
f the
Dig
ital F
light
Gui
danc
e (D
FGS
) Sys
tem
s
SP
EC
IAL
NO
TE: C
MR
No
22-1
.aA
IRP
LAN
E N
OTE
: App
licab
le o
nly
to a
utol
and
oper
ator
s on
ly.
For t
he D
FGC
-971
and
sub
sequ
ent c
onfig
urat
ions
, the
DFG
S R
TS n
eed
only
be
perfo
rmed
on
a si
ngle
DFG
C. F
or D
FGC
-972
with
KC
N K
1123
(SB
MD
80-2
2-11
3) in
stal
led,
the
DFG
S R
TS is
not
requ
ired.
U71
22-0
01-0
122
-10-
00-7
108
OP
C2
A2
A44
4501
A0.
06O
pera
tiona
l Che
ck o
f the
Dis
enga
ge A
ural
War
ning
AIR
PLA
NE
NO
TE: A
pplic
able
onl
y to
aut
olan
d op
erat
ors
only
, if n
ot o
pera
tiona
l fo
r all
fligh
t pha
ses.
U72
22-0
01-0
222
-10-
00-7
109
OP
C1
C1
C44
0.16
Ope
ratio
nal C
heck
of t
he G
o A
roun
d S
elec
tion
(Sin
gle
TOG
O s
witc
h op
erat
ion)
U73
22-0
01-0
322
-10-
00-7
108
OP
C1
C1
C44
0.02
Ope
ratio
nal C
heck
of t
he A
ltitu
de A
lert
Sys
tem
(If 7
50 fe
et A
ural
War
ning
E
nabl
e no
t ins
talle
d)
U74
22-0
02-0
022
-10-
01-2
10G
VI
1000
0 FH
1000
0 FH
5151
02A
0.10
Gen
eral
Vis
ual I
nspe
ctio
n of
the
Ele
vato
r Aut
opilo
t Ser
vo T
orqu
e Li
mite
r Dua
l S
prin
gs
SP
EC
IAL
NO
TE: C
MR
No
22-1
.b.1
AIR
PLA
NE
NO
TE: A
pplic
able
onl
y to
aut
olan
d op
erat
ors
only
.
U75
22-0
03-0
022
-10-
01-2
11D
ET
1000
0 FH
1000
0 FH
5151
02A
0.20
Det
aile
d V
isua
l Ins
pect
ion
of th
e E
leva
tor A
utop
ilot S
ervo
Tor
que
Lim
iter
Pus
hrod
Ass
embl
y
SP
EC
IAL
NO
TE: C
MR
No
22-1
.b.2
AIR
PLA
NE
NO
TE: A
pplic
able
onl
y to
aut
olan
d op
erat
ors
only
.
U76
22-0
04-0
022
-01-
01-7
10O
PC
2500
FH
2500
FH
440.
09O
pera
tiona
l Che
ck o
f the
Thr
ust C
utba
ck S
yste
m
SP
EC
IAL
NO
TE: C
MR
No
34-3
Rev 0 19 March 2014
2-14
MD-80 MAINTENANCE MANUAL
BO
EIN
G P
RO
PR
IETA
RY
- C
opyr
ight
© U
npub
lishe
d W
ork
- See
title
pag
e fo
r det
ails
AU
GU
ST
2013
ME
80-0
20-T
NK
PA
GE
1.1
-7
0 1 2 3 4 5
DC
-9-8
0SF
Mai
nten
ance
Pla
nnin
g D
ocum
ent
SYST
EMS
AN
D P
OW
ERPL
AN
T M
AIN
TEN
AN
CE
PRO
GR
AM
MPD
ITEM
NU
MB
ERAM
M
REF
EREN
CE
C A T
T A S K
INTE
RVA
L
THR
ES.
REP
EAT
TASK
DES
CR
IPTI
ON
ZON
EAC
CES
SM
AN-
HO
UR
S
77A
TA 2
3: C
OM
MU
NIC
ATI
ON
S
U78
23-0
30-0
123
-30-
00-7
208
FNC
4 C
4 C
44 580.
38Fu
nctio
nal C
heck
of t
he P
asse
nger
Add
ress
Spe
aker
Sys
tem
U79
23-0
30-0
223
-30-
00-7
108
OP
C2
C2
C44 58
0.12
Ope
ratio
nal C
heck
of t
he P
A P
riorit
y S
yste
m
U80
23-0
60-0
123
-60-
00-7
206
FNC
2 C
2 C
10 30 60
0.58
Func
tiona
l Che
ck o
f the
Sta
tic D
isch
argi
ng C
apab
ility
U81
23-0
71-0
123
-70-
00-7
109
OP
C1
C1
C44 57
5716
C0.
08O
pera
tiona
l Che
ck o
f the
Coc
kpit
Voi
ce R
ecor
ding
Sys
tem
for 4
cha
nnel
op
erat
ion
U82
23-0
71-0
223
-70-
03-9
019
DIS
6 Y
R6
YR
5757
16C
0.08
Rep
lace
Voi
ce R
ecor
der U
nder
wat
er L
ocat
or B
eaco
n B
atte
ry
83A
TA 2
4: E
LEC
TRIC
AL
POW
ER
U84
24-0
01-0
024
-23-
02-9
01D
IS10
YR
NO
TE10
YR
NO
TE44
2.00
Dis
card
the
Em
erge
ncy
Pow
er S
witc
h (S
1-14
8). (
SC
I 24-
1)
AIR
PLA
NE
NO
TE: T
his
task
is a
pplic
able
to a
ircra
ft eq
uipp
ed w
ith E
ME
R P
WR
sw
itch
P/N
103
-220
0.IN
TER
VA
L N
OTE
: Usi
ng th
e A
MO
C in
SC
I 24-
1 fo
r rec
alcu
latio
n of
the
inte
rval
fo
r rep
laci
ng th
e E
mer
genc
y P
ower
Sw
itch,
a 1
0 ye
ar in
terv
al w
as s
elec
ted.
U85
24-0
01-0
124
-10-
02-2
127
GV
I1
AN
OTE
1 A
NO
TE71 72
7705
C78
06C
0.10
Insp
ect C
SD
Cha
rge
and
Sca
veng
e Fi
lter D
iffer
entia
l Pre
ssur
e In
dica
tors
INTE
RV
AL
NO
TE: P
er M
anuf
actu
rer's
Life
Lim
it
U86
24-0
01-0
224
-10-
01-7
109
OP
CE
NG
CN
GE
NG
CN
G44 71 72
0.07
Ope
ratio
nal C
heck
of t
he C
SD
Dis
conn
ect S
yste
m
U87
24-0
01-0
324
-20-
00-7
108
OP
CE
NG
CN
GE
NG
CN
G44
0.12
Ope
ratio
nal C
heck
of t
he E
NG
Gen
erat
or F
ield
Dis
conn
ect
U88
24-0
01-0
724
-30-
01-9
028
RS
T1
C1
C45
4501
A0.
25R
esto
ratio
n of
the
Mai
n A
ircra
ft B
atte
ries
U89
24-0
01-0
824
-20-
00-7
109
OP
C2
C2
C44
0.25
Ope
ratio
nal C
heck
of t
he L
oad
She
d fo
r Gen
erat
ors
U90
24-0
01-0
924
-20-
01-7
109
OP
C4
C4
C44 45 46
4501
A0.
08O
pera
tiona
l Che
ck o
f the
AC
Cro
sstie
Loc
kout
Ale
rt
U91
24-0
01-1
024
-30-
03-7
109
OP
C2
C2
C44 45
4501
A0.
07O
pera
tiona
l Che
ck o
f the
Mec
hani
cal R
emot
e 80
am
p. C
/B re
set
U92
24-0
01-1
124
-20-
00-7
108
OP
C1
C1
C44
0.12
Ope
ratio
nal C
heck
of t
he A
PU
Gen
erat
or F
ield
Dis
conn
ect
U93
24-0
01-1
224
-41-
01-2
119
DE
T3
C3
C43
0.06
Det
aile
d In
spec
tion
of th
e E
xter
nal P
ower
Rec
epta
cle
(Inte
rnal
)
U94
24-0
01-1
324
-41-
01-7
209
FNC
3 C
3 C
430.
06Fu
nctio
nal C
heck
of t
he E
xter
nal P
ower
Rec
epta
cle
Stu
ds w
ith a
GO
/NO
-GO
G
age
Rev 0 19 March 2014
2-15
MD-80 MAINTENANCE MANUAL
BO
EIN
G P
RO
PR
IETA
RY
- C
opyr
ight
© U
npub
lishe
d W
ork
- See
title
pag
e fo
r det
ails
AU
GU
ST
2013
ME
80-0
20-T
NK
PA
GE
1.1
-8
0 1 2 3 4 5
DC
-9-8
0SF
Mai
nten
ance
Pla
nnin
g D
ocum
ent
SYST
EMS
AN
D P
OW
ERPL
AN
T M
AIN
TEN
AN
CE
PRO
GR
AM
MPD
ITEM
NU
MB
ERAM
M
REF
EREN
CE
C A T
T A S K
INTE
RVA
L
THR
ES.
REP
EAT
TASK
DES
CR
IPTI
ON
ZON
EAC
CES
SM
AN-
HO
UR
S
U95
24-9
21-6
024
-23-
02-7
20FN
C1
C1
C44
0.17
Torq
ue C
heck
of t
he E
mer
genc
y P
ower
Sw
itch
Term
inal
s.
AIR
PLA
NE
NO
TE: A
nytim
e w
ork
is p
erfo
rmed
in th
e fo
rwar
d ov
erhe
ad s
witc
h pa
nel.
96A
TA 2
5: E
QU
IPM
ENT/
FUR
NIS
HIN
GS
U97
25-0
15-0
125
-13-
01-2
1125
-13-
02-2
115
DE
T1
C1
C44
0.08
Det
aile
d In
spec
tion
of th
e C
rew
Sea
tbel
t Con
nect
ing
Link
s
U98
25-0
15-0
212
-21-
03-6
406
LUB
1 C
1 C
440.
08Lu
bric
ate
Flig
ht C
ompa
rtmen
t Sea
ts a
nd S
eat T
rack
s
U99
25-0
15-0
325
-13-
01-7
108
OP
C1
C1
C44
0.08
Ope
ratio
nal C
heck
of t
he C
apta
in's
and
Firs
t Offi
cer's
Iner
tial R
eel
U10
0
25-0
15-0
405
-21-
01-2
105
GV
I1
C1
C44
0.02
Gen
eral
Vis
ual I
nspe
ctio
n of
the
Flig
ht C
ompa
rtmen
t Sea
tbel
ts a
nd R
otar
y B
uckl
e A
ssem
bly
U10
1
25-0
15-0
505
-21-
01-2
115
DE
T2
C2
C44
0.17
Det
aile
d In
spec
tion
of th
e C
rew
Sea
ts a
ttach
men
ts, t
rack
s an
d lo
ckin
g to
st
ruct
ure
U10
2
25-0
15-0
605
-21-
01-2
115
DE
T1
C1
C44
0.08
Det
aile
d in
spec
tion
of th
e cr
ew s
eat b
elt a
ttach
bol
t for
gen
eral
sec
urity
and
at
tach
men
t.
U10
3
25-0
23-0
125
-23-
04-2
118
DE
T2
C2
C58
0.03
Det
aile
d In
spec
tion
of th
e P
asse
nger
Sea
ts fo
r atta
chm
ent a
nd lo
ckin
g to
st
ruct
ure
U10
4
25-0
23-0
225
-23-
01-2
118
DE
T2
C2
C46
0.14
Det
aile
d In
spec
tion
of th
e Fo
rwar
d, M
id a
nd A
ft A
ttend
ant S
eats
for a
ttach
men
t an
d lo
ckin
g to
stru
ctur
e
U10
5
25-0
23-0
405
-21-
01-2
108
GV
I2
C2
C46 58
0.01
Gen
eral
Vis
ual I
nspe
ctio
n of
the
Pas
seng
er S
eat B
elt W
ebbi
ng&
Flig
ht A
ttend
ant
Sea
t Bel
t/Sho
ulde
r Har
ness
Web
bing
&S
hack
le A
ssem
bly
U10
6
25-0
23-0
505
-21-
01-2
118
DE
T2
C2
C44 58
0.21
Det
aile
d In
spec
tion
of th
e P
ass&
FA S
eat B
elt A
ttach
Bol
t Ass
embl
y fo
r C
ondi
tion
and
Sec
urity
U10
7
25-0
23-0
625
-23-
01-7
205
FNC
1 C
1 C
460.
05Fu
nctio
nal C
heck
of t
he F
oldi
ng A
ttend
ant H
ydra
ulic
/Pne
umat
ic S
eat S
nubb
er
U10
8
25-0
23-0
725
-23-
01-2
115
DE
T1
C1
C46
0.02
Det
aile
d In
spec
tion
of th
e Fo
rwar
d an
d A
ft A
ttend
ant S
eat H
ydra
ulic
/Pne
umat
ic
Snu
bber
U10
925
-023
-08
25-2
3-01
-710
8O
PC
1 C
1 C
460.
02O
pera
tiona
l Che
ck o
f the
Flig
ht A
ttend
ant S
houl
der H
arne
ss/In
ertia
l Ree
l
U11
0
25-0
50-0
105
-21-
01-2
108
GV
I1
A1
A51 57
2.00
Gen
eral
Vis
ual I
nspe
ctio
n of
the
Car
go C
ompa
rtmen
t Lin
ing.
U11
1
25-0
60-0
325
-62-
04-7
108
OP
C1
CN
OTE
1 C
NO
TE46 58 61
0.66
Ope
ratio
nal C
heck
of t
he D
oor a
nd T
ailc
one
Slid
e D
eplo
ymen
t Sys
tem
INTE
RV
AL
NO
TE: O
n a
rota
ting
basi
s, a
diff
eren
t doo
r will
be s
elec
ted
each
in
terv
al.
U11
2
25-0
60-0
525
-62-
00-2
1225
-62-
01-2
129
VC
K1
A1
A46 58 61
0.05
Vis
ual c
heck
of t
he e
vacu
atio
n sl
ide
bottl
e fo
r pro
per p
ress
ure.
Rev 0 19 March 2014
2-16
MD-80 MAINTENANCE MANUAL
BO
EIN
G P
RO
PR
IETA
RY
- C
opyr
ight
© U
npub
lishe
d W
ork
- See
title
pag
e fo
r det
ails
AU
GU
ST
2013
ME
80-0
20-T
NK
PA
GE
1.1
-9
0 1 2 3 4 5
DC
-9-8
0SF
Mai
nten
ance
Pla
nnin
g D
ocum
ent
SYST
EMS
AN
D P
OW
ERPL
AN
T M
AIN
TEN
AN
CE
PRO
GR
AM
MPD
ITEM
NU
MB
ERAM
M
REF
EREN
CE
C A T
T A S K
INTE
RVA
L
THR
ES.
REP
EAT
TASK
DES
CR
IPTI
ON
ZON
EAC
CES
SM
AN-
HO
UR
S
R11
3
25-0
60-0
625
-62-
00-9
029
RS
T36
MO
1 Y
RN
OTE
36 M
O1
YR
NO
TE
460.
18R
esto
ratio
n of
the
esca
pe s
lides
.
INTE
RV
AL
NO
TE: 3
yea
rs u
ntil
15 y
ears
, the
n 1
year
.If
the
infla
tabl
e, h
ose,
and
app
licab
le li
fe-li
mite
d ite
ms
are
repl
aced
at 1
5 ye
ars,
th
en th
e st
anda
rd 3
yea
r mai
nten
ance
inte
rval
is re
-inst
ated
for t
he n
ext 1
5 ye
ars.
U11
425
-060
-07
25-6
1-00
-211
9D
ET
2 C
2 C
440.
17D
etai
led
insp
ectio
n of
the
esca
pe li
nes
(coc
kpit
and
cabi
n).
U11
5
25-0
60-0
925
-60-
02-2
128
VC
K1
A1
A46 58
0.05
Vis
ual c
heck
of t
he fi
rst a
id k
its fo
r ins
pect
ion
date
and
sea
l.
U11
6
25-0
60-1
025
-60-
02-9
018
DIS
1 A
1 A
46 580.
02D
isca
rd m
edic
al k
it tim
e lim
ited
supp
lies.
U11
7
25-0
60-1
125
-64-
01-2
1125
-64-
03-2
118
DE
T1
C1
C44 46 58
0.81
Det
aile
d in
spec
tion
of th
e lif
e ve
st e
xpira
tion
date
.
U11
8
25-0
60-2
025
-60-
00-7
109
OP
C1
A1
A46 58
0.03
Ope
ratio
nal c
heck
of t
he fl
ashl
ight
s.
U11
9
25-0
60-2
125
-60-
00-9
019
DIS
3 D
Y3
DY
46 580.
08D
isca
rd th
e fla
shlig
ht b
atte
ries.
U12
0
25-0
60-2
225
-62-
00-9
0125
-62-
01-9
019
DIS
VE
N R
EC
VE
N R
EC
46 58 61
0.38
Dis
card
the
esca
pe s
lide
bottl
es.
U12
1
25-0
60-2
525
-64-
01-9
0225
-64-
03-9
029
RS
TV
EN
RE
CV
EN
RE
C44 46 58 61
0.04
Res
tora
tion
of th
e lif
e ve
sts.
U12
2
25-0
60-2
625
-60-
02-2
12V
CK
1 A
1 A
46 580.
02V
isua
l che
ck o
f the
med
ical
kits
for i
nspe
ctio
n da
te a
nd s
eal.
123
ATA
26:
FIR
E PR
OTE
CTI
ON
U12
4
26-0
12-0
126
-10-
06-7
108
OP
C1
C1
C44 45 59
5909
C0.
06O
pera
tiona
l Che
ck o
f the
AP
U E
xter
nal F
ire W
arni
ng H
orn
and
Rem
ote
Pan
el
Ligh
t
U12
526
-012
-02
12-2
1-03
-640
9LU
B1
C1
C59
5909
C0.
08Lu
bric
ate
the
AP
U F
ire W
arni
ng H
orn
(If a
pplic
able
)
U12
6
26-0
21-0
126
-20-
01-7
109
OP
C2
C2
C44 59
5909
C0.
10O
pera
tiona
l Che
ck o
f the
Fire
x B
ottle
Low
Pre
ssur
e S
witc
hes
and
Ligh
ts b
y m
anua
l tes
tU
127
26-0
21-0
326
-20-
03-9
019
DIS
10 Y
R10
YR
5961
01A
0.08
Dis
card
Dis
char
ge C
artri
dge
U12
8
26-0
21-0
426
-20-
03-7
109
OP
C2
C2
C44 59
6101
A0.
41O
pera
tiona
l Che
ck o
f the
Age
nt D
isch
arge
Sys
tem
to c
heck
Firi
ng C
ircui
t In
tegr
ity
Rev 0 19 March 2014
2-17
MD-80 MAINTENANCE MANUAL
BO
EIN
G P
RO
PR
IETA
RY
- C
opyr
ight
© U
npub
lishe
d W
ork
- See
title
pag
e fo
r det
ails
AU
GU
ST
2013
ME
80-0
20-T
NK
PA
GE
1.1
-10
0 1 2 3 4 5
DC
-9-8
0SF
Mai
nten
ance
Pla
nnin
g D
ocum
ent
SYST
EMS
AN
D P
OW
ERPL
AN
T M
AIN
TEN
AN
CE
PRO
GR
AM
MPD
ITEM
NU
MB
ERAM
M
REF
EREN
CE
C A T
T A S K
INTE
RVA
L
THR
ES.
REP
EAT
TASK
DES
CR
IPTI
ON
ZON
EAC
CES
SM
AN-
HO
UR
S
U12
9
26-0
21-0
505
-21-
01-2
108
GV
I2
C2
C59 61 81 82
8101
C81
03C
8105
C81
11C
8113
C81
15C
8202
C82
04C
8206
C82
12C
8214
C82
16C
1.00
Gen
eral
Vis
ual I
nspe
ctio
n of
the
Eng
ine
and
AP
U F
ire E
xtin
guis
hing
D
eplo
ymen
t Lin
es.
U13
0
26-0
21-0
626
-10-
07-7
108
OP
C2
C2
C44 59
5903
A59
04A
0.41
Ope
ratio
nal C
heck
of t
he A
PU
Em
erge
ncy
Shu
tdow
n S
yste
m fr
om th
e C
ockp
it an
d E
xter
nal P
anel
U13
1
26-0
21-0
826
-20-
04-7
20FN
C2
C2
C59 61 81 82
NO
TE0.
75Fu
nctio
nal C
heck
of t
he F
ire E
xtin
guis
hing
Fle
x H
oses
for t
he E
ngin
es a
nd
AP
U.
AC
CE
SS
NO
TE: A
cces
s to
the
depl
oym
ent l
ines
is th
roug
h th
e en
gine
pyl
on
door
s, p
ylon
apr
on d
oors
, AP
U c
ompa
rtmen
t doo
rs a
nd ta
ilcon
e ac
cess
doo
r.
U13
2
26-0
23-0
126
-20-
05-2
119
DE
T1
C1
C44 46 58
0.33
Det
aile
d In
spec
tion
of th
e H
alon
and
Wat
er P
orta
ble
Fire
Ext
ingu
ishe
rs fo
r pr
oper
wei
ght a
nd c
ondi
tion
U13
3
26-0
23-0
226
-20-
05-2
129
VC
K1
A1
A44 46 58
0.02
Vis
ual C
heck
the
Hal
on P
orta
ble
Fire
Ext
ingu
ishe
rs fo
r pro
per p
ress
ure
U13
4
26-0
23-0
326
-20-
05-2
108
GV
I1
A1
A44 46 58
0.04
Gen
eral
Vis
ual I
nspe
ctio
n of
the
Por
tabl
e Fi
re E
xtin
guis
hers
&B
rack
ets
U13
5
26-0
23-0
726
-20-
05-9
019
DIS
VE
N R
EC
VE
N R
EC
44 46 58
0.05
Dis
card
the
Hal
on a
nd C
O2
Por
tabl
e Fi
re e
xtin
guis
her B
ottle
s
136
ATA
27:
FLI
GH
T C
ON
TRO
LS
U13
7
27-0
01-0
027
-30-
01-2
11D
ET
1 C
1 C
4544
32A
0.08
Det
aile
d In
spec
tion
of th
e E
leva
tor V
aria
ble
Load
-Fee
l and
Cen
terin
g S
prin
g M
echa
nism
Tor
que
Tube
Rev 0 19 March 2014
2-18
MD-80 MAINTENANCE MANUAL
BO
EIN
G P
RO
PR
IETA
RY
- C
opyr
ight
© U
npub
lishe
d W
ork
- See
title
pag
e fo
r det
ails
AU
GU
ST
2013
ME
80-0
20-T
NK
PA
GE
1.1
-11
0 1 2 3 4 5
DC
-9-8
0SF
Mai
nten
ance
Pla
nnin
g D
ocum
ent
SYST
EMS
AN
D P
OW
ERPL
AN
T M
AIN
TEN
AN
CE
PRO
GR
AM
MPD
ITEM
NU
MB
ERAM
M
REF
EREN
CE
C A T
T A S K
INTE
RVA
L
THR
ES.
REP
EAT
TASK
DES
CR
IPTI
ON
ZON
EAC
CES
SM
AN-
HO
UR
S
D13
8
27-0
02-0
027
-20-
12-2
50S
DI
3500
FC
NO
TE35
00 F
CN
OTE
4542
01A
4302
A44
10C
4415
A44
34C
3.00
Edd
y C
urre
nt a
nd V
isua
l Ins
pect
ion
of th
e C
apta
in's
and
Firs
t Offi
cer's
Rud
der
Ped
al A
djus
ter H
ub
INTE
RV
AL
NO
TE: C
ompl
ianc
e w
ith S
/B D
C9-
27-0
325
cons
titut
es a
term
inat
ing
actio
n fo
r thi
s in
spec
tion.
U13
9
27-0
03-0
027
-00-
00-7
10FN
C25
00 F
H25
00 F
H44
0.08
Per
form
a ta
ke-o
ff w
arni
ng o
pera
tiona
l tes
t, th
e fla
p ha
ndle
/flap
thum
bwhe
el
war
ning
sw
itch,
hor
izon
tal s
tabi
lizer
gre
en b
and
switc
h an
d gr
ound
sen
sing
rela
y fu
nctio
ns a
re v
erifi
ed g
ood.
SP
EC
IAL
NO
TE: C
MR
No
27-1
U14
0
27-0
11-0
120
-10-
17-2
116
DE
T1
C1
C15 16 55 56
0.42
Det
aile
d In
spec
tion
of th
e A
ilero
n C
ontro
l Cab
les
(Exp
osed
Are
a)
U14
1
27-0
11-0
220
-10-
17-2
116
DE
T4
C4
C45 51 53
0.33
Det
aile
d In
spec
tion
of th
e A
ilero
n C
ontro
l Cab
les
(Une
xpos
ed A
rea)
U14
2
27-0
11-0
327
-10-
09-7
206
FNC
4 C
4 C
44 45 55 56
0.05
Func
tiona
l Che
ck o
f the
Aile
ron
Con
trol T
orqu
e Tu
be a
nd O
verri
de M
echa
nism
U14
3
27-0
11-0
412
-21-
02-6
406
LUB
4 A
4 A
15 160.
16Lu
bric
ate
the
Left
and
Rig
ht A
ilero
n C
ontro
l Tab
Pus
hrod
s, C
ontro
l Mec
hani
sm
Hin
ges
and
Con
trol T
ab H
inge
s
U14
4
27-0
11-0
512
-21-
02-6
406
LUB
1 C
1 C
55 5645
01A
0.10
Lubr
icat
e th
e A
ilero
n S
ecto
r and
Pul
ley
Bea
ring
on th
e La
tera
l Con
trol m
ixer
s
U14
527
-011
-06
12-2
1-03
-640
6LU
B1
C1
C44
0.03
Lubr
icat
e th
e C
ontro
l Whe
el B
earin
gs
U14
6
27-0
12-0
120
-10-
17-2
116
DE
T1
C1
C15 16 55 56
0.42
Det
aile
d In
spec
tion
of th
e A
ilero
n Tr
im C
able
s (E
xpos
ed a
rea)
U14
7
27-0
12-0
220
-10-
17-2
116
DE
T4
C4
C45 51 53
0.33
Det
aile
d In
spec
tion
of th
e A
ilero
n Tr
im C
able
s (U
nexp
osed
are
a)
U14
8
27-0
12-0
312
-21-
02-6
406
LUB
4 A
4 A
15 160.
16Lu
bric
ate
the
Left
and
Rig
ht A
ilero
n Tr
im T
ab P
ushr
ods,
Trim
Tab
Act
uato
rs a
nd
Trim
Tab
Hin
ges
Rev 0 19 March 2014
2-19
MD-80 MAINTENANCE MANUAL
BO
EIN
G P
RO
PR
IETA
RY
- C
opyr
ight
© U
npub
lishe
d W
ork
- See
title
pag
e fo
r det
ails
AU
GU
ST
2013
ME
80-0
20-T
NK
PA
GE
1.1
-12
0 1 2 3 4 5
DC
-9-8
0SF
Mai
nten
ance
Pla
nnin
g D
ocum
ent
SYST
EMS
AN
D P
OW
ERPL
AN
T M
AIN
TEN
AN
CE
PRO
GR
AM
MPD
ITEM
NU
MB
ERAM
M
REF
EREN
CE
C A T
T A S K
INTE
RVA
L
THR
ES.
REP
EAT
TASK
DES
CR
IPTI
ON
ZON
EAC
CES
SM
AN-
HO
UR
S
U14
9
27-0
21-0
120
-10-
17-2
116
DE
T4
C4
C45 51 53 57 59 61
0.52
Det
aile
d In
spec
tion
of th
e R
udde
r Con
trol C
able
s an
d Tr
im C
able
s (U
nexp
osed
A
rea)
U15
0
27-0
21-0
212
-21-
02-6
406
LUB
4 A
4 A
61 65N
OTE
0.19
Lubr
icat
e R
udde
r Hin
ges,
Rud
der T
ab H
inge
s an
d C
ontro
l Mec
hani
sm
AC
CE
SS
NO
TE: R
efer
to C
hapt
er 0
6 of
you
r AM
M fo
r Alu
min
um o
r Com
posi
te
Rud
der a
cces
s pa
nels
.
U15
1
27-0
23-0
127
-20-
09-7
109
OP
C2
C2
C44
0.03
Ope
ratio
nal C
heck
of t
he R
udde
r Hyd
raul
ic S
hut o
ff sy
stem
and
man
ual
reve
rsio
n m
ode
U15
2
27-0
31-0
120
-10-
17-2
116
DE
T4
C4
C31 32 45 51 53 57 58 59 61 63 65
1.13
Det
aile
d In
spec
tion
of th
e E
leva
tor C
able
s S
yste
m (U
nexp
osed
Are
a)
U15
3
27-0
31-0
212
-21-
02-6
406
LUB
4 A
4 A
35 3633
19A
3420
A35
07A
3513
A35
17A
3519
A35
29A
3608
A36
14A
3618
A36
20A
3630
A
0.17
Lubr
icat
e th
e E
leva
tor A
ssem
bly
U15
4
27-0
33-0
127
-30-
11-7
209
FNC
4 C
4 C
5959
02C
0.13
Func
tiona
l Che
ck o
f the
Ele
vato
r Hyd
raul
ic S
yste
m to
mai
ntai
n pr
essu
re w
ithou
t M
ain
Hyd
raul
ic S
yste
m p
ress
ure
Rev 0 19 March 2014
2-20
MD-80 MAINTENANCE MANUAL
BO
EIN
G P
RO
PR
IETA
RY
- C
opyr
ight
© U
npub
lishe
d W
ork
- See
title
pag
e fo
r det
ails
AU
GU
ST
2013
ME
80-0
20-T
NK
PA
GE
1.1
-13
0 1 2 3 4 5
DC
-9-8
0SF
Mai
nten
ance
Pla
nnin
g D
ocum
ent
SYST
EMS
AN
D P
OW
ERPL
AN
T M
AIN
TEN
AN
CE
PRO
GR
AM
MPD
ITEM
NU
MB
ERAM
M
REF
EREN
CE
C A T
T A S K
INTE
RVA
L
THR
ES.
REP
EAT
TASK
DES
CR
IPTI
ON
ZON
EAC
CES
SM
AN-
HO
UR
S
U15
5
27-0
41-0
220
-10-
17-2
116
DE
T4
C4
C44 45 51 53 57 59 61 64 65
0.62
Det
ail I
nspe
ctio
n of
the
Hor
izon
tal S
tabi
lizer
Con
trol a
nd In
dica
tion
Cab
les
(Une
xpos
ed A
rea)
U15
627
-041
-03
27-4
0-00
-710
9O
PC
2 C
2 C
440.
03O
pera
tiona
l Che
ck o
f the
Bra
ke O
verri
de S
witc
h
U15
7
27-0
41-0
427
-40-
04-9
01R
ST
1600
0 FH
1600
0 FH
51N
OTE
0.33
Rem
ove
and
repl
ace
prim
ary
long
itudi
nal u
p/do
wn
cont
acto
rs w
ith O
EM
ov
erha
uled
or n
ew.
AIR
PLA
NE
NO
TE: F
or a
ircra
ft w
ith re
lays
man
ufac
ture
d by
Lea
ch a
nd a
re p
art
num
ber 5
D03
55-1
or 9
207-
1029
6.A
CC
ES
S N
OTE
: Due
to m
ultip
le c
onfig
urat
ions
, ref
er to
AM
M C
hapt
er 0
6 fo
r ac
cess
pan
el.
U15
8
27-0
42-0
127
-40-
01-7
109
OP
C1
C1
C63
NO
TE0.
05O
pera
tiona
l Che
ck o
f the
Hor
izon
tal S
tabi
lizer
Prim
ary
Trim
Mot
or H
eate
r (If
Inst
alle
d)
AC
CE
SS
NO
TE: R
efer
to A
MM
Cha
pter
06
for a
cces
s pa
nels
.
U15
9
27-0
51-0
120
-10-
17-2
116
DE
T1
C1
C15 16 55 56
0.36
Det
aile
d In
spec
tion
of th
e Fl
ap C
able
Sys
tem
in th
e ex
pose
d ar
ea (E
xpos
ed
Are
a)
U16
0
27-0
51-0
220
-10-
17-2
116
DE
T4
C4
C45 51
0.26
Det
aile
d In
spec
tion
of th
e Fl
ap C
able
Sys
tem
in th
e (U
nexp
osed
Are
a)
U16
1
27-0
51-0
312
-21-
02-6
406
LUB
4 A
4 A
15 160.
26Lu
bric
ate
the
left
and
right
Fla
p Fe
ed B
ack
Driv
e Li
nkag
e
U16
2
27-0
55-0
112
-21-
02-6
406
LUB
4 A
4 A
15 160.
16Lu
bric
ate
the
Eig
ht F
lap
Hyd
raul
ic A
ctua
ting
Cyl
inde
rs, R
olle
r Bea
rings
and
Fo
llow
-up
Link
age
U16
3
27-0
61-0
127
-60-
00-7
108
OP
C1
C1
C44
0.08
Ope
ratio
nal C
heck
of t
he "S
PO
ILE
R D
EP
LOY
ED
", "A
UTO
SP
OIL
ER
FA
IL" o
r "A
UTO
SP
OIL
ER
DO
NO
T U
SE
" Ind
icat
ion
U16
427
-061
-02
27-6
0-00
-710
9O
PC
1 C
1 C
440.
05O
pera
tiona
l Che
ck o
f the
"SP
OIL
ER
FLA
P E
XTE
ND
" Ind
icat
ion
U16
527
-062
-01
27-6
0-00
-710
7O
PC
1 C
1 C
440.
17O
pera
tiona
l Che
ck o
f the
Aut
ospo
iler S
yste
m (R
TO F
unct
ion
only
)
U16
6
27-0
63-0
120
-10-
17-2
116
DE
T1
C1
C15 16 55 56
0.43
Det
aile
d In
spec
tion
of th
e S
poile
r Spe
edbr
ake
and
Flig
ht S
poile
r cab
les
(exp
osed
are
a)
Rev 0 19 March 2014
2-21
MD-80 MAINTENANCE MANUAL
BO
EIN
G P
RO
PR
IETA
RY
- C
opyr
ight
© U
npub
lishe
d W
ork
- See
title
pag
e fo
r det
ails
AU
GU
ST
2013
ME
80-0
20-T
NK
PA
GE
1.1
-14
0 1 2 3 4 5
DC
-9-8
0SF
Mai
nten
ance
Pla
nnin
g D
ocum
ent
SYST
EMS
AN
D P
OW
ERPL
AN
T M
AIN
TEN
AN
CE
PRO
GR
AM
MPD
ITEM
NU
MB
ERAM
M
REF
EREN
CE
C A T
T A S K
INTE
RVA
L
THR
ES.
REP
EAT
TASK
DES
CR
IPTI
ON
ZON
EAC
CES
SM
AN-
HO
UR
S
U16
7
27-0
63-0
220
-10-
17-2
119
DE
T4
C4
C45 51 53
0.33
Det
aile
d In
spec
tion
of th
e S
poile
r/Spe
edbr
ake
cabl
es (U
nexp
osed
are
a)
U16
8
27-0
63-0
327
-62-
13-7
109
OP
C4
C4
C55 56
0.33
Ope
ratio
nal C
heck
of t
he G
roun
d S
poile
r Ove
rride
pus
hrod
U16
9
27-0
63-0
412
-21-
02-6
406
LUB
4 A
4 A
15 1615
25A
1526
A15
27A
1625
A16
26A
1627
A
0.17
Lubr
icat
e G
roun
d S
poile
r Act
uato
r Cra
nks,
Con
trol R
od E
nds,
Idle
r Lin
ks, D
rive
Link
s A
ttach
Pin
s an
d Fi
tting
, Driv
e Li
nk A
ssem
bly
Bol
ts D
rive
Hin
ge F
ittin
gs
and
Driv
e D
rum
Axi
s B
earin
g
U17
0
27-0
67-0
112
-21-
02-6
406
LUB
4 A
4 A
15 1615
25A
1526
A15
27A
1625
A16
26A
1627
A
0.17
Lubr
icat
e th
e G
roun
d S
poile
r Cyl
inde
rs a
nd S
poile
r Act
uato
rs
U17
1
27-0
81-0
120
-10-
17-2
116
DE
T4
C4
C45 51 53
0.33
Det
aile
d In
spec
tion
of th
e Fl
ap /
Sla
t Com
man
d C
able
Loo
p (U
nexp
osed
Are
a)
U17
227
-081
-02
05-2
1-01
-210
6G
VI
4 A
4 A
5151
07C
0.08
Gen
eral
Vis
ual I
nspe
ctio
n of
the
Sla
t Driv
e M
echa
nism
Rev 0 19 March 2014
2-22
MD-80 MAINTENANCE MANUAL
BO
EIN
G P
RO
PR
IETA
RY
- C
opyr
ight
© U
npub
lishe
d W
ork
- See
title
pag
e fo
r det
ails
AU
GU
ST
2013
ME
80-0
20-T
NK
PA
GE
1.1
-15
0 1 2 3 4 5
DC
-9-8
0SF
Mai
nten
ance
Pla
nnin
g D
ocum
ent
SYST
EMS
AN
D P
OW
ERPL
AN
T M
AIN
TEN
AN
CE
PRO
GR
AM
MPD
ITEM
NU
MB
ERAM
M
REF
EREN
CE
C A T
T A S K
INTE
RVA
L
THR
ES.
REP
EAT
TASK
DES
CR
IPTI
ON
ZON
EAC
CES
SM
AN-
HO
UR
S
U17
3
27-0
81-0
312
-21-
02-6
406
LUB
4 A
4 A
11 12 51
1110
C11
12C
1114
C11
16C
1118
C11
21C
1122
C11
23C
1124
C11
28C
1130
C11
34C
1148
C11
59C
1161
C11
62C
1164
C11
66C
1167
C11
69C
1170
C11
73C
1174
C11
83C
1209
C12
10C
1212
C12
14C
1218
C12
21C
1222
C12
35C
1236
C12
43C
1250
C12
53C
1254
C12
55C
1256
C
0.44
Lubr
icat
ion
of th
e S
lat D
rive
Sys
tem
U17
427
-081
-04
20-1
0-17
-211
6D
ET
4 C
4 C
510.
12D
etai
led
Insp
ectio
n of
the
Sla
t Fol
low
-up
cabl
es (U
nexp
osed
Are
a)
Rev 0 19 March 2014
2-23
MD-80 MAINTENANCE MANUAL
BO
EIN
G P
RO
PR
IETA
RY
- C
opyr
ight
© U
npub
lishe
d W
ork
- See
title
pag
e fo
r det
ails
AU
GU
ST
2013
ME
80-0
20-T
NK
PA
GE
1.1
-16
0 1 2 3 4 5
DC
-9-8
0SF
Mai
nten
ance
Pla
nnin
g D
ocum
ent
SYST
EMS
AN
D P
OW
ERPL
AN
T M
AIN
TEN
AN
CE
PRO
GR
AM
MPD
ITEM
NU
MB
ERAM
M
REF
EREN
CE
C A T
T A S K
INTE
RVA
L
THR
ES.
REP
EAT
TASK
DES
CR
IPTI
ON
ZON
EAC
CES
SM
AN-
HO
UR
S
U17
5
27-0
81-0
505
-21-
01-2
116
DE
T2
C2
C11 12 51
1110
C11
11C
1112
C11
13C
1114
C11
15C
1116
C11
17C
1118
C11
19C
1120
C11
22C
1131
C11
32C
1136
C11
44C
1160
C11
63C
1165
C11
68C
1171
C11
73C
1174
C11
85C
1210
C12
11C
1212
C12
13C
1214
C12
15C
1217
C12
18C
1219
C12
20C
1222
C12
26C
1231
C12
42C
1244
C
0.66
Det
aile
d In
spec
tion
of th
e S
lat D
rive
Trac
ks a
nd S
lat D
rive
Cab
les
176
ATA
28:
FU
EL
Rev 0 19 March 2014
2-24
MD-80 MAINTENANCE MANUAL
BO
EIN
G P
RO
PR
IETA
RY
- C
opyr
ight
© U
npub
lishe
d W
ork
- See
title
pag
e fo
r det
ails
AU
GU
ST
2013
ME
80-0
20-T
NK
PA
GE
1.1
-17
0 1 2 3 4 5
DC
-9-8
0SF
Mai
nten
ance
Pla
nnin
g D
ocum
ent
SYST
EMS
AN
D P
OW
ERPL
AN
T M
AIN
TEN
AN
CE
PRO
GR
AM
MPD
ITEM
NU
MB
ERAM
M
REF
EREN
CE
C A T
T A S K
INTE
RVA
L
THR
ES.
REP
EAT
TASK
DES
CR
IPTI
ON
ZON
EAC
CES
SM
AN-
HO
UR
S
U17
7
28-0
11-0
128
-10-
02-2
118
DE
T8
C8
C13 14
1307
C13
11C
1410
C14
14C
0.20
Det
aile
d In
spec
tion
of th
e Fu
el T
ank
Flap
per C
heck
Val
ves
U17
8
28-0
12-0
128
-10-
06-2
1128
-10-
08-2
1128
-10-
09-2
11
8 9D
ET
8 C
8 C
13 14 23
1307
C13
23C
1333
C14
10C
1426
C14
36C
0.23
Det
aile
d In
spec
tion
of th
e V
ent R
elie
f and
Clim
b V
ent F
loat
Val
ves
U17
9
28-0
12-0
328
-10-
11-2
119
DE
T8
C8
C13 14 23
1307
C13
33C
1410
C14
36C
0.25
Det
aile
d In
spec
tion
of th
e V
ent D
rain
Sw
ing
Che
ck V
alve
s
U18
0
28-0
12-0
528
-10-
07-2
118 9
DE
T8
C8
C13 14
1323
C14
26C
0.17
Det
aile
d In
spec
tion
of th
e Fu
el T
ank
Ven
t Sys
tem
Fla
me
Arre
stor
R18
1
28-0
13-0
128
-10-
05-2
119
DE
T8
C8
C13 14
1357
C14
36C
1456
C
0.25
Det
aile
d In
spec
tion
of th
e W
ing
Tank
Sca
veng
e C
heck
Val
ves
U18
2
28-0
13-0
228
-10-
13-9
0228
-10-
14-9
029
RS
T8
C8
C13 14 23
1307
C14
10C
1436
C
0.25
Cle
an th
e Ta
nk S
cave
nge
Filte
rs
U18
3
28-0
13-0
328
-10-
16-9
029
RS
T8
C8
C13 14 23
1307
C14
10C
2301
C23
02C
0.25
Cle
an th
e sc
aven
ge ra
kes.
(SFA
R 8
8)
U18
428
-013
-04
28-1
0-05
-720
9FN
C8
C8
C23
1436
C0.
25Fu
nctio
nal C
heck
of t
he C
ente
r Tan
k C
heck
Val
ve
U18
5
28-0
22-0
228
-42-
00-7
108
OP
C2
C2
C12 13 14 44
0.50
Ope
ratio
nal C
heck
of t
he "F
UE
L LE
VE
L LO
W" a
lert
and
latc
hing
circ
uit
U18
628
-022
-03
28-4
1-00
-710
8O
PC
4 C
4 C
440.
16O
pera
tiona
l Che
ck o
f the
"CTR
FU
EL
PR
ES
LO
W "
Ale
rt in
hibi
t Sys
tem
U18
728
-022
-04
71-0
0-00
-710
8O
PC
1 C
1 C
440.
50O
pera
tiona
l Che
ck o
f the
Suc
tion
Feed
Sys
tem
U18
8
28-0
24-0
128
-20-
00-7
209
FNC
4 C
4 C
55 56 60
0.09
Func
tiona
l Che
ck o
f the
Fue
l Shr
oud
Sys
tem
U18
9
28-0
24-0
328
-20-
00-7
209
OP
C4
C4
C55 56 60
0.02
Ope
ratio
nal C
heck
of t
he D
rain
Mas
t ass
embl
y (V
entin
g)
Rev 0 19 March 2014
2-25
MD-80 MAINTENANCE MANUAL
BO
EIN
G P
RO
PR
IETA
RY
- C
opyr
ight
© U
npub
lishe
d W
ork
- See
title
pag
e fo
r det
ails
AU
GU
ST
2013
ME
80-0
20-T
NK
PA
GE
1.1
-18
0 1 2 3 4 5
DC
-9-8
0SF
Mai
nten
ance
Pla
nnin
g D
ocum
ent
SYST
EMS
AN
D P
OW
ERPL
AN
T M
AIN
TEN
AN
CE
PRO
GR
AM
MPD
ITEM
NU
MB
ERAM
M
REF
EREN
CE
C A T
T A S K
INTE
RVA
L
THR
ES.
REP
EAT
TASK
DES
CR
IPTI
ON
ZON
EAC
CES
SM
AN-
HO
UR
S
190
ATA
29:
HYD
RA
ULI
C P
OW
ER
U19
1
29-0
01-0
029
-01-
01-2
11D
ET
5000
FH
NO
TE50
00 F
HN
OTE
55 560.
50D
etai
led
Insp
ectio
n of
the
Aux
iliary
Hyd
raul
ic P
ump
Pow
er F
eede
r Wiri
ng (A
LI
20-2
)
INTE
RV
AL
NO
TE: M
DC
-92K
9145
U19
2
29-0
12-0
129
-10-
01-7
209
FNC
2 C
2 C
55 561.
00Fu
nctio
nal C
heck
of t
he M
ain
Hyd
raul
ic R
eser
voirs
for i
nter
nal l
eaka
ge
U19
3
29-0
12-0
227
-20-
15-6
1427
-30-
11-6
1478
-31-
01-6
14
9S
VC
1 A
1 A
5959
01C
5902
C61
01A
0.03
Ser
vice
the
Rud
der,
Ele
vato
r and
the
Thru
st R
ever
ser H
ydra
ulic
Acc
umul
ator
to
prop
er c
harg
e
U19
4
29-0
12-0
329
-10-
14-2
119
DE
T1
A1
A55 56 59
0.05
Det
aile
d In
spec
tion
of th
e D
elta
-P In
dica
tor o
n H
ydra
ulic
Filt
ers
U19
5
29-0
21-0
129
-10-
06-2
116
DE
T1
A1
A56
0.02
Det
aile
d In
spec
tion
of th
e A
uxilia
ry H
ydra
ulic
Pum
p S
eal D
rain
Con
tain
er fo
r flu
id d
ue to
loss
of s
eal
U19
6
29-0
22-0
129
-10-
07-2
119
DE
T1
A1
A55
0.02
Det
aile
d In
spec
tion
of th
e Tr
ansf
er P
ump
Sea
l Dra
in C
onta
iner
for f
luid
due
to
loss
of s
eal
U19
7
29-0
22-0
229
-10-
08-7
209
FNC
1 C
1 C
44 55 56
0.25
Func
tiona
l che
ck o
f the
hyd
raul
ic p
ower
tran
sfer
uni
t (P
TU) s
huto
ff sy
stem
.
U19
8
29-0
32-0
129
-30-
00-2
119
DE
T1
C1
C44 55 56
0.02
Det
aile
d In
spec
tion
of th
e co
ckpi
t ind
icat
ion
and
rese
rvoi
r lev
el fo
r acc
urac
y
199
ATA
30:
ICE
AN
D R
AIN
PR
OTE
CTI
ON
U20
0
30-0
01-0
030
-10-
15-2
00V
CK
NO
TEN
OTE
13 140.
50In
spec
tions
of t
he O
verw
ing
Ice
Pro
tect
ion
Hea
ter B
lank
ets
INTE
RV
AL
NO
TE: R
efer
to M
D80
-30-
071
for r
epet
itive
inte
rval
s.
N20
1
30-0
02-0
030
-10-
00-2
11D
ET
1 C
1 C
13 140.
50D
etai
led
insp
ectio
n of
the
over
win
g ic
e pr
otec
tion
heat
er b
lank
et a
ssem
bly
for
dent
/pun
ctur
e an
d ed
ge s
eala
nt c
ondi
tion
and
secu
rity.
N20
2
30-0
03-0
030
-10-
00-2
80S
DI
5 C
5 C
13 148.
00S
peci
al D
etai
led
Insp
ectio
n of
the
LH/R
H O
verw
ing
Ice
Pro
tect
ion
Hea
ter
Bla
nket
Ass
embl
y fo
r Voi
ds.
N20
3
30-0
04-0
030
-10-
00-7
20FN
C2
C2
C51
1.25
Func
tiona
l Che
ck o
f the
LH
/RH
Ove
rwin
g Ic
e P
rote
ctio
n B
lank
et H
eate
r Con
trol
Uni
t.
U20
4
30-0
10-0
130
-10-
11-7
109
OP
C3
C3
C45 51 55 56
5116
C51
27C
0.27
Ope
ratio
nal C
heck
of t
he A
irfoi
l Ant
i-Ici
ng 1
30 D
eg O
verh
eat S
enso
rs
Rev 0 19 March 2014
2-26
MD-80 MAINTENANCE MANUAL
BO
EIN
G P
RO
PR
IETA
RY
- C
opyr
ight
© U
npub
lishe
d W
ork
- See
title
pag
e fo
r det
ails
AU
GU
ST
2013
ME
80-0
20-T
NK
PA
GE
1.1
-19
0 1 2 3 4 5
DC
-9-8
0SF
Mai
nten
ance
Pla
nnin
g D
ocum
ent
SYST
EMS
AN
D P
OW
ERPL
AN
T M
AIN
TEN
AN
CE
PRO
GR
AM
MPD
ITEM
NU
MB
ERAM
M
REF
EREN
CE
C A T
T A S K
INTE
RVA
L
THR
ES.
REP
EAT
TASK
DES
CR
IPTI
ON
ZON
EAC
CES
SM
AN-
HO
UR
S
U20
5
30-0
10-0
230
-10-
11-7
109
OP
C3
C3
C11 12 51 55 56 57
NO
TE1.
20O
pera
tiona
l Che
ck o
f the
Airf
oil A
nti-I
cing
180
Deg
Ove
rhea
t Sen
sors
AC
CE
SS
NO
TE: R
efer
to A
MM
Cha
pter
06
for p
rope
r acc
ess
pane
l.
U20
6
30-0
10-0
330
-10-
06-7
209
FNC
2 C
2 C
590.
27Fu
nctio
nal C
heck
of t
he A
irfoi
l Ant
i-Ici
ng 5
00 D
eg "H
IGH
TE
MP
" Sen
sors
and
A
lerts
U20
7
30-0
10-0
430
-10-
06-7
209
FNC
3 C
3 C
44 590.
27Fu
nctio
nal C
heck
of t
he A
irfoi
l Ant
i-Ici
ng 3
00/3
90 D
eg "T
EM
P L
OW
" Sen
sors
an
d A
lerts
U20
8
30-0
10-0
530
-10-
10-7
209
FNC
3 C
3 C
44 590.
13Fu
nctio
nal C
heck
of t
he A
irfoi
l Ant
i-Ici
ng T
ail L
ow P
ress
ure
Sw
itch
and
Sys
tem
A
lerts
U20
9
30-0
10-0
630
-10-
10-7
209
FNC
6 C
6 C
44 5151
07C
5138
C0.
13Fu
nctio
nal C
heck
of t
he A
irfoi
l Ant
i-Ici
ng W
ing
Low
Pre
ssur
e S
witc
h an
d S
yste
m
Ale
rts
U21
0
30-0
10-0
730
-10-
06-7
108
OP
C2
C2
C44
0.13
Ope
ratio
nal C
heck
of t
he A
irfoi
l Ant
i-Ici
ng "L
/R IC
E P
RO
T TE
MP
LO
W" a
lerts
an
d in
hibi
t circ
uit
U21
1
30-0
10-0
830
-10-
05-7
209
FNC
6 C
6 C
44 590.
10Fu
nctio
nal C
heck
of t
he A
irfoi
l Ant
i-Ici
ng S
uppl
y P
ress
ure
Hig
h S
witc
h an
d S
yste
m A
lerts
U21
2
30-0
30-0
130
-30-
01-7
109
OP
C1
C1
C44 50
0.03
Ope
ratio
nal C
heck
of t
he A
ltern
ate
Sta
tic P
ort H
eate
rs
213
ATA
31:
INST
RU
MEN
TS
U21
4
31-0
31-0
131
-31-
01-7
209
FNC
1 C
1 C
44 570.
10Fu
nctio
nal C
heck
of a
ll R
equi
red
Airc
raft
Par
amet
ers
Bei
ng R
ecor
ded
Pro
perly
by
the
Flig
ht R
ecor
der
SP
EC
IAL
NO
TE: T
his
item
has
two
proc
edur
es. T
he O
pera
tor m
ay p
erfo
rm
eith
er p
roce
dure
to s
atis
fy th
e re
quire
men
t.A
IRP
LAN
E N
OTE
: Rec
ordi
ng o
f par
amet
ers
and
tole
ranc
es s
peci
fied
by T
itle
14
CFR
, Par
t 121
App
endi
x B
or L
ocal
Reg
ulat
ory
Req
uire
men
ts m
ust b
e ve
rifie
d
U21
5
31-0
31-0
231
-31-
12-9
019
DIS
6 Y
R6
YR
5757
16C
0.02
Rep
lace
Flig
ht D
ata
Rec
orde
r Und
erw
ater
Loc
ator
Bea
con
(ULB
) Bat
tery
U21
631
-051
-01
31-5
1-00
-710
8O
PC
1 C
1 C
440.
05O
pera
tiona
l Che
ck th
e La
ndin
g G
ear A
ural
war
ning
U21
731
-051
-02
27-0
0-00
-710
8O
PC
1 A
1 A
440.
08O
pera
tiona
l Che
ck th
e Ta
ke-o
ff W
arni
ng S
yste
m
U21
831
-051
-03
31-5
1-00
-710
8O
PC
2 C
2 C
440.
25O
pera
tiona
l Che
ck th
e S
lat O
vers
peed
Aur
al w
arni
ng
U21
931
-051
-04
31-5
1-00
-710
8O
PC
2 C
2 C
440.
25O
pera
tiona
l Che
ck th
e O
vers
peed
Aur
al w
arni
ng
220
ATA
32:
LA
ND
ING
GEA
R
U22
1
32-0
11-0
105
-21-
01-2
105
GV
I1
A1
A17 18
1.00
Gen
eral
Vis
ual I
nspe
ctio
n of
the
Mai
n La
ndin
g G
ear S
hock
Stru
ts.
Rev 0 19 March 2014
2-27
MD-80 MAINTENANCE MANUAL
BO
EIN
G P
RO
PR
IETA
RY
- C
opyr
ight
© U
npub
lishe
d W
ork
- See
title
pag
e fo
r det
ails
AU
GU
ST
2013
ME
80-0
20-T
NK
PA
GE
1.1
-20
0 1 2 3 4 5
DC
-9-8
0SF
Mai
nten
ance
Pla
nnin
g D
ocum
ent
SYST
EMS
AN
D P
OW
ERPL
AN
T M
AIN
TEN
AN
CE
PRO
GR
AM
MPD
ITEM
NU
MB
ERAM
M
REF
EREN
CE
C A T
T A S K
INTE
RVA
L
THR
ES.
REP
EAT
TASK
DES
CR
IPTI
ON
ZON
EAC
CES
SM
AN-
HO
UR
S
U22
2
32-0
11-0
332
-00-
00-9
025
RS
T12
0 M
O12
0 M
O17 18
20.6
0R
esto
re th
e Le
ft an
d R
ight
Mai
n La
ndin
g G
ear S
hock
Stru
ts, U
pper
Sid
e B
race
, Lo
wer
Sid
e B
race
, Fix
ed S
ide
Bra
ces,
Upp
er L
ock
Link
, Low
er L
ock
Link
and
U
pper
and
Low
er T
orqu
e Li
nks.
U22
3
32-0
11-0
432
-00-
00-9
015
DIS
NO
TEN
OTE
17 180.
01D
isca
rd th
e Le
ft an
d R
ight
Mai
n La
ndin
g G
ear C
ompo
nent
s.
INTE
RV
AL
NO
TE: P
/N 5
9353
49 L
ink
Ass
embl
y - U
pper
Loc
k 48
,000
FC
P/N
593
7032
Bra
cket
Ass
embl
y - B
unge
e 48
,000
FC
P/N
593
5848
-1 M
ain
Stru
t Ass
embl
y - F
ixed
Sid
e Li
nk 5
5,00
0P
/N 5
9358
48-5
01 M
ain
Stru
t Ass
embl
y - F
ixed
Sid
e Li
nk 1
50,0
00P
er M
cDon
nell
Dou
glas
DC
-9/M
D-8
0 S
afe
Life
Lim
itsN
ote
3, T
ype
Cer
tific
ate
Dat
a S
heet
No.
A6W
ER
epor
t # M
DC
-J00
05, D
ated
01-
Dec
-200
2
U22
4
32-0
11-0
512
-21-
04-6
405 6
LUB
2 A
2 A
17 18 55 56
2.00
Lubr
icat
e al
l Fitt
ings
on
the
Left
and
Rig
ht M
ain
Land
ing
Gea
r Ass
embl
y an
d D
oors
U22
5
32-0
13-0
205
-21-
01-2
105
GV
I1
A1
A55 56
0.50
Gen
eral
Vis
ual I
nspe
ctio
n of
the
Mai
n La
ndin
g G
ear U
pper
Sid
e B
race
, Low
er
Sid
e B
race
, Fix
ed S
ide
Bra
ces,
Upp
er L
ock
Link
, Low
er L
ock
Link
, and
Lef
t, R
ight
, Upp
er a
nd L
ower
Tor
que
Link
s.
U22
6
32-0
13-0
532
-11-
06-2
126
GV
I1
A1
A17 18
0.17
Insp
ect t
he L
eft a
nd R
ight
Mai
n La
ndin
g G
ear H
ydra
ulic
Dam
pers
for f
luid
leve
l
U22
7
32-0
21-0
332
-00-
00-9
025
RS
T12
0 M
O12
0 M
O47
9.83
Res
tore
the
Nos
e La
ndin
g G
ear S
hock
Stru
t, C
ylin
der,
Hou
sing
, Ste
erin
g Le
ver,
Pis
ton,
Axl
e, U
pper
Dra
g B
race
, Low
er D
rag
Bra
ce, U
pper
Loc
k Li
nk, L
ower
Lo
ck L
ink
and
Upp
er a
nd L
ower
Tor
que
Link
s.
U22
8
32-0
21-0
432
-00-
00-9
015
DIS
NO
TEN
OTE
470.
01D
isca
rd th
e N
ose
Land
ing
Gea
r Com
pone
nts.
INTE
RV
AL
NO
TE: P
/N 3
9144
64-5
07 L
ink
Ass
embl
y - U
pper
Loc
k 46
,500
FC
P/N
391
4464
-511
Lin
k A
ssem
bly
- Upp
er L
ock
46,5
00 F
CP
/N 3
9139
68 L
ink
Ass
embl
y - L
ower
Loc
k 59
,333
FC
P/N
595
4183
-1 H
ousi
ng A
ssem
bly
20,0
00 F
CN
ote:
Whe
n th
e 59
2707
9 ho
usin
g is
rew
orke
d to
repa
ir th
e re
tract
arm
per
D
raw
ing
5954
183.
Per
McD
onne
ll D
ougl
as D
C-9
/MD
-80
Saf
e Li
fe L
imits
Not
e 3,
Typ
e C
ertif
icat
e D
ata
She
et N
o. A
6WE
Rep
ort #
MD
C-J
0005
, Dat
ed 0
1-D
ec-2
002
U22
9
32-0
21-0
512
-21-
04-6
405 6
LUB
2 A
2 A
470.
60Lu
bric
ate
the
Nos
e La
ndin
g G
ear,
Spr
ay D
efle
ctor
s, a
nd D
oors
Rev 0 19 March 2014
2-28
MD-80 MAINTENANCE MANUAL
BO
EIN
G P
RO
PR
IETA
RY
- C
opyr
ight
© U
npub
lishe
d W
ork
- See
title
pag
e fo
r det
ails
AU
GU
ST
2013
ME
80-0
20-T
NK
PA
GE
1.1
-21
0 1 2 3 4 5
DC
-9-8
0SF
Mai
nten
ance
Pla
nnin
g D
ocum
ent
SYST
EMS
AN
D P
OW
ERPL
AN
T M
AIN
TEN
AN
CE
PRO
GR
AM
MPD
ITEM
NU
MB
ERAM
M
REF
EREN
CE
C A T
T A S K
INTE
RVA
L
THR
ES.
REP
EAT
TASK
DES
CR
IPTI
ON
ZON
EAC
CES
SM
AN-
HO
UR
S
U23
0
32-0
22-0
205
-21-
01-2
105
GV
I1
A1
A47
0.25
Gen
eral
Vis
ual I
nspe
ctio
n of
the
Nos
e La
ndin
g G
ear U
pper
Dra
g B
race
, Low
er
Dra
g B
race
, Upp
er L
ock
Link
s, L
ower
Loc
k Li
nk, a
nd U
pper
and
Low
er T
orqu
e Li
nks.
U23
1
32-0
24-0
232
-23-
01-2
116
DE
T4
C4
C43 47
0.17
Det
aile
d In
spec
tion
of th
e G
roun
d S
ense
Cab
le S
yste
m (U
nexp
osed
Are
a)
U23
232
-031
-01
20-1
0-17
-211
6D
ET
1 C
1 C
560.
08D
etai
led
Insp
ectio
n of
the
Land
ing
Gea
r Con
trol C
able
s (E
xpos
ed A
rea)
U23
3
32-0
31-0
220
-10-
17-2
116
DE
T4
C4
C42 45 51 53
0.33
Det
aile
d In
spec
tion
of th
e La
ndin
g G
ear C
ontro
l Cab
les
(Une
xpos
ed A
rea)
U23
432
-031
-03
20-1
0-17
-211
6D
ET
1 C
1 C
430.
08D
etai
led
Insp
ectio
n of
the
Ant
i-Ret
ract
Cab
le S
yste
m (E
xpos
ed A
rea)
U23
532
-031
-04
20-1
0-17
-211
6D
ET
4 C
4 C
420.
08D
etai
led
Insp
ectio
n of
the
Ant
i-Ret
ract
Cab
le S
yste
m (U
nexp
osed
Are
a)
U23
632
-031
-05
32-3
1-02
-710
8O
PC
2 C
2 C
440.
16O
pera
tiona
l Che
ck o
f the
Alte
rnat
e G
ear E
xten
d S
yste
m
U23
7
32-0
31-0
620
-10-
17-2
118
DE
T1
C1
C43 56
0.08
Det
aile
d In
spec
tion
of th
e La
ndin
g G
ear A
ltern
ate
Con
trol C
able
s (E
xpos
ed
Are
a)
U23
8
32-0
31-0
720
-10-
17-2
118
DE
T4
C4
C42 45 51 53
0.33
Det
aile
d In
spec
tion
of th
e La
ndin
g G
ear A
ltern
ate
cont
rol C
able
s (U
nexp
osed
A
rea)
U23
9
32-0
35-0
105
-21-
01-2
106 8
GV
I1
A1
A47
0.25
Gen
eral
Vis
ual I
nspe
ctio
n of
the
Nos
e La
ndin
g G
ear R
etra
ct C
ylin
der,
Bun
gee
Spr
ings
Bun
gee
Cyl
inde
r and
Loc
k P
ins.
U24
0
32-0
35-0
332
-31-
02-7
108
OP
C2
C2
C47
0.03
Ope
ratio
nal C
heck
of t
he N
ose
Land
ing
Gea
r Alte
rnat
e C
ontro
l Sys
tem
(Fre
e fa
ll)
U24
1
32-0
41-0
105
-21-
01-2
105
GV
I1
A1
A17 18
0.20
Gen
eral
Vis
ual I
nspe
ctio
n of
the
Mai
n La
ndin
g G
ear W
heel
s an
d Ti
res.
U24
2
32-0
41-0
232
-40-
01-2
505
SD
I24
MO
1800
FC
NO
TE
24 M
O18
00 F
CN
OTE
17 180.
67S
peci
al D
etai
l Ins
pect
ion
of th
e M
ain
Land
ing
Gea
r Whe
els
INTE
RV
AL
NO
TE: W
hich
ever
occ
urs
first
.
U24
332
-042
-01
05-2
1-01
-210
5G
VI
1 A
1 A
470.
25G
ener
al V
isua
l Ins
pect
ion
of th
e N
ose
Land
ing
Gea
r Whe
els
and
Tire
s.
U24
4
32-0
43-0
132
-40-
00-7
208
FNC
1 A
1 A
17 180.
03Fu
nctio
nal C
heck
the
Mai
n La
ndin
g G
ear B
rake
pin
s fo
r bra
ke w
ear
U24
5
32-0
44-0
132
-42-
02-7
205
FNC
2 C
2 C
55 560.
17Fu
nctio
nal C
heck
of t
he D
ual B
rake
Con
trol V
alve
s
U24
632
-044
-02
05-2
1-01
-210
5G
VI
1 C
1 C
450.
08G
ener
al V
isua
l Ins
pect
ion
of th
e B
rake
Ped
al M
echa
nica
l Lin
kage
U24
7
32-0
44-0
320
-10-
17-2
115
DE
T1
C1
C55 56
0.17
Det
aile
d In
spec
tion
of th
e B
rake
Ped
al C
ontro
l Cab
les
(Exp
osed
Are
a)
U24
8
32-0
44-0
420
-10-
17-2
115
DE
T4
C4
C45 51 53
0.33
Det
aile
d In
spec
tion
of th
e B
rake
Ped
al C
ontro
l Cab
les
(Une
xpos
ed A
rea)
Rev 0 19 March 2014
2-29
MD-80 MAINTENANCE MANUAL
BO
EIN
G P
RO
PR
IETA
RY
- C
opyr
ight
© U
npub
lishe
d W
ork
- See
title
pag
e fo
r det
ails
AU
GU
ST
2013
ME
80-0
20-T
NK
PA
GE
1.1
-22
0 1 2 3 4 5
DC
-9-8
0SF
Mai
nten
ance
Pla
nnin
g D
ocum
ent
SYST
EMS
AN
D P
OW
ERPL
AN
T M
AIN
TEN
AN
CE
PRO
GR
AM
MPD
ITEM
NU
MB
ERAM
M
REF
EREN
CE
C A T
T A S K
INTE
RVA
L
THR
ES.
REP
EAT
TASK
DES
CR
IPTI
ON
ZON
EAC
CES
SM
AN-
HO
UR
S
U24
9
32-0
44-0
505
-21-
01-2
105
GV
I1
C1
C55 56
0.17
Gen
eral
Vis
ual I
nspe
ctio
n of
the
Bra
ke P
ress
ure
Man
ifold
s
U25
0
32-0
44-0
605
-21-
01-2
105
GV
I1
C1
C44 45
0.03
Gen
eral
Vis
ual I
nspe
ctio
n of
the
Par
king
Bra
ke M
echa
nism
U25
1
32-0
44-0
732
-42-
10-7
205
FNC
2 C
2 C
55 560.
33Fu
nctio
nal c
heck
of t
he b
rake
de-
spin
cyl
inde
rs. (
SFA
R 8
8)
U25
2
32-0
44-0
932
-42-
04-6
109
SV
C1
A1
A55 56
0.07
Ser
vice
the
Bra
ke S
yste
m A
ccum
ulat
ors
U25
332
-045
-01
32-4
3-03
-710
8O
PC
2 C
2 C
441.
03O
pera
tiona
l Che
ck o
f the
Dua
l Ant
i-Ski
d C
ontro
l Val
ves
U25
4
32-0
45-0
232
-43-
03-9
028
RS
T12
0 M
O12
0 M
O55 56
0.01
Res
tore
the
Dua
l Ant
i-Ski
d C
ontro
l Val
ve A
ssem
bly
U25
5
32-0
51-0
232
-51-
00-2
116
DE
T1
C1
C44 45
4201
A43
02A
0.17
Det
aile
d In
spec
tion
of th
e S
teer
ing
Whe
el, D
rum
, cab
les
and
rudd
er p
edal
st
eerin
g ca
bles
(Exp
osed
Are
a)
U25
6
32-0
70-0
132
-70-
00-6
14G
VI
4 C
4 C
60 611.
00S
ervi
ce c
heck
of t
he T
ail B
umpe
r Stru
t Nitr
ogen
Cha
rge
per M
D-8
0 S
ervi
ce
Lette
r MD
-80-
SL-
32-1
07.
U25
7
32-0
70-0
232
-70-
00-6
10S
VC
8 C
8 C
60 611.
50S
ervi
ce th
e Ta
il B
umpe
r Stru
t Nitr
ogen
Cha
rge
and
Oil
per M
D-8
0 S
ervi
ce L
ette
r M
D-8
0-S
L-32
-107
258
ATA
33:
LIG
HTS
U25
9
33-0
01-0
021
-31-
09-7
20FN
C50
00 F
H50
00 F
H58
0.50
Per
form
a fu
nctio
nal c
heck
of t
he a
uto
air-c
ondi
tioni
ng p
ack
shut
dow
n&la
ndin
g lig
ht re
tract
sys
tem
.
SP
EC
IAL
NO
TE: C
MR
No
33-1
U26
0
33-0
02-0
033
-41-
02-6
40LU
B2
A2
A11 12
0.25
Lubr
icat
e th
e W
ing
Land
ing
Ligh
ts S
ecto
r Gea
r and
Wor
m P
inio
n
U26
1
33-0
14-0
133
-51-
00-7
108
OP
C1
C1
C44
0.01
Ope
ratio
nal C
heck
of E
mer
genc
y P
ower
Sw
itch
to v
erify
ope
ratio
n C
ockp
it Fl
ood
Ligh
ts
U26
2
33-0
14-0
233
-51-
00-7
108
OP
C1
C1
C44
0.01
Ope
ratio
nal C
heck
of C
ockp
it Fl
ood
Ligh
ts b
y pu
lling
Em
erge
ncy
Bus
Sen
sing
C
ircui
t Bre
aker
U26
3
33-0
32-0
133
-30-
00-7
108
OP
C1
A1
A58
0.01
Ope
ratio
nal C
heck
of t
he M
ain
Whe
el W
ell L
ight
s us
ing
Cab
in F
loor
Sw
itch
U26
433
-041
-03
33-4
1-01
-901
DIS
2500
0 FH
2500
0 FH
440.
25D
isca
rd th
e N
ose
Land
ing
Gea
r Lan
ding
and
Tax
i Lig
ht S
witc
h
U26
533
-042
-01
33-4
3-01
-710
9O
PC
1 A
1 A
440.
02O
pera
tiona
l Che
ck W
ing
Stro
be L
ight
s
U26
633
-042
-02
33-4
2-01
-710
9O
PC
1 A
1 A
440.
02O
pera
tiona
l Che
ck A
nti-C
ollis
ion
Ligh
ts
U26
733
-042
-03
33-4
3-01
-710
9O
PC
1 A
1 A
440.
02O
pera
tiona
l Che
ck P
ositi
on L
ight
s
U26
8
33-0
42-0
405
-21-
01-2
119
DE
T1
A1
A11 12
0.03
Det
aile
d In
spec
tion
of th
e P
ositi
on L
ight
Len
ses
for c
razi
ng w
hich
cau
ses
diffu
sion
of l
ight
sou
rce
U26
9
33-0
51-0
133
-53-
00-7
108
OP
C2
A2
A44 50 61
0.03
Ope
ratio
nal C
heck
of t
he E
mer
genc
y Li
ghtin
g S
yste
m o
pera
ted
from
the
Flig
ht
Dec
k an
d Fl
ight
Atte
ndan
t pos
ition
Rev 0 19 March 2014
2-30
MD-80 MAINTENANCE MANUAL
BO
EIN
G P
RO
PR
IETA
RY
- C
opyr
ight
© U
npub
lishe
d W
ork
- See
title
pag
e fo
r det
ails
AU
GU
ST
2013
ME
80-0
20-T
NK
PA
GE
1.1
-23
0 1 2 3 4 5
DC
-9-8
0SF
Mai
nten
ance
Pla
nnin
g D
ocum
ent
SYST
EMS
AN
D P
OW
ERPL
AN
T M
AIN
TEN
AN
CE
PRO
GR
AM
MPD
ITEM
NU
MB
ERAM
M
REF
EREN
CE
C A T
T A S K
INTE
RVA
L
THR
ES.
REP
EAT
TASK
DES
CR
IPTI
ON
ZON
EAC
CES
SM
AN-
HO
UR
S
U27
0
33-0
51-0
233
-53-
00-9
028
RS
T1
C1
C57 58
0.33
Rep
lace
bat
terie
s in
Em
erge
ncy
Ligh
t Bat
tery
Pac
ks
271
ATA
34:
NA
VIG
ATI
ON
N27
2
34-0
01-0
034
-11-
00-7
20FN
C48
MO
48 M
O42 44
0.50
Per
form
a F
unct
iona
l Che
ck o
f the
Cap
tain
and
Firs
t Offi
cer's
Alti
met
er (S
CI 3
4-1)
.
AIR
PLA
NE
NO
TE: A
pplie
s to
airc
raft
appr
oved
for f
lyin
g R
educ
ed V
ertic
al
Sep
arat
ion
Min
imum
(RV
SM
) airs
pace
.
U27
3
34-0
10-0
134
-11-
00-2
128
GV
I1
C1
C45 59
4501
A0.
28In
spec
t the
Pito
t and
Sta
tic S
yste
m fo
r wat
er
U27
434
-010
-02
34-1
1-02
-210
6G
VI
4 A
4 A
630.
10G
ener
al V
isua
l Ins
pect
ion
of th
e R
udde
r Pito
t Pro
be
U27
5
34-0
10-0
334
-11-
00-7
206
FNC
2 C
2 C
440.
50Fu
nctio
nal C
heck
of t
he P
itot a
nd S
tatic
Sys
tem
for l
eaka
ge (H
igh
Alti
tude
)
U27
6
34-0
10-0
434
-11-
03-7
109
OP
C2
C2
C40 44
0.50
Ope
ratio
nal C
heck
of t
he S
tatic
Sel
ecto
r Sys
tem
U27
734
-010
-05
34-1
6-03
-710
6O
PC
1 C
1 C
440.
08O
pera
tiona
l Che
ck o
f the
Air
Dat
a S
witc
hing
U27
8
34-0
10-0
634
-11-
00-7
206
FNC
2 C
2 C
40 440.
17Fu
nctio
nal C
heck
of t
he S
tand
by A
ltim
eter
/Airs
peed
Sys
tem
U27
9
34-0
10-0
734
-11-
01-2
118
DE
T3
YR
3 Y
R50
0.10
Det
aile
d In
spec
tion
of th
e S
tatic
Por
ts
AIR
PLA
NE
NO
TE: (
RV
SM
Ope
ratio
n on
ly)
U28
034
-022
-01
34-2
2-06
-710
9O
PC
1 C
1 C
440.
03O
pera
tiona
l Che
ck o
f the
EFI
S S
ourc
e S
witc
hing
U28
1
34-0
23-0
134
-23-
00-7
109
OP
C1
C1
C42
0.08
Ope
ratio
nal C
heck
of t
he A
ttitu
de S
witc
hing
AIR
PLA
NE
NO
TE: I
f ins
talle
d.
U28
2
34-0
29-0
134
-21-
01-2
118
DE
T1
C1
C44
0.03
Det
aile
d In
spec
tion
of th
e S
tand
by C
ompa
ss fo
r lea
ks a
nd fr
eedo
m o
f m
ovem
ent o
f the
Com
pass
Car
dU
283
34-0
29-0
234
-21-
01-2
118
DE
T4
C4
C44
0.02
Det
aile
d In
spec
tion
of th
e S
tand
by C
ompa
ss c
lam
ps a
nd b
rack
ets
U28
434
-029
-03
34-2
1-01
-720
8FN
C4
C4
C44
2.00
Func
tiona
l Che
ck o
f the
Sta
ndby
Com
pass
for C
alib
ratio
n
U28
534
-032
-02
34-5
1-01
-211
9D
ET
4 C
4 C
630.
16D
etai
led
Insp
ectio
n of
the
VO
R/N
AV
Ant
enna
for p
rope
r bon
ding
U28
634
-046
-01
34-4
6-00
-720
8FN
C1
C1
C44
0.75
Func
tiona
l Che
ck o
f the
TC
AS
Sys
tem
U28
7
34-0
54-0
134
-54-
00-7
206
FNC
24 M
ON
OTE
24 M
ON
OTE
441.
00Fu
nctio
nal C
heck
of t
he A
ir Tr
affic
Con
trol (
ATC
) Sys
tem
AIR
PLA
NE
NO
TE: T
ask
is a
pplic
able
to U
.S. o
pera
tors
onl
y, b
y N
atio
nal
requ
irem
ent.
INTE
RV
AL
NO
TE: P
er F
AR
91.
413
or L
ocal
Reg
ulat
ory
Req
uire
men
ts
288
ATA
35:
OXY
GEN
Rev 0 19 March 2014
2-31
MD-80 MAINTENANCE MANUAL
BO
EIN
G P
RO
PR
IETA
RY
- C
opyr
ight
© U
npub
lishe
d W
ork
- See
title
pag
e fo
r det
ails
AU
GU
ST
2013
ME
80-0
20-T
NK
PA
GE
1.1
-24
0 1 2 3 4 5
DC
-9-8
0SF
Mai
nten
ance
Pla
nnin
g D
ocum
ent
SYST
EMS
AN
D P
OW
ERPL
AN
T M
AIN
TEN
AN
CE
PRO
GR
AM
MPD
ITEM
NU
MB
ERAM
M
REF
EREN
CE
C A T
T A S K
INTE
RVA
L
THR
ES.
REP
EAT
TASK
DES
CR
IPTI
ON
ZON
EAC
CES
SM
AN-
HO
UR
S
U28
9
35-0
10-0
235
-10-
01-2
126
GV
I1
A1
A44
0.01
Vis
ual C
heck
of t
he C
rew
Oxy
gen
Bot
tle P
ress
ure
Gau
ge fo
r pro
per p
ress
ure
U29
0
35-0
10-0
335
-10-
01-7
206
FNC
4 C
4 C
440.
33Fu
nctio
nal C
heck
of t
he C
rew
Oxy
gen
Dem
and
and
Sup
ply
Pre
ssur
e R
egul
ator
s
U29
135
-010
-04
35-1
0-00
-211
6D
ET
1 C
1 C
440.
08D
etai
led
Insp
ectio
n of
the
Cre
w O
xyge
n M
ask
and
Mic
Ass
embl
y
U29
235
-010
-08
35-1
0-03
-710
9O
PC
1 A
1 A
440.
08O
pera
tiona
l Che
ck o
f the
Oxy
gen
Mas
k M
icro
phon
e
U29
3
35-0
10-1
035
-10-
00-2
119
DE
T1
C1
C44
0.08
Det
aile
d In
spec
tion
of th
e S
mok
e G
oggl
es, S
mok
e H
ood,
Ful
l Fac
e O
2 M
ask
and
Sm
oke
Mas
k
U29
4
35-0
10-1
135
-10-
01-9
019
DIS
NO
TEN
OTE
440.
25D
isca
rd th
e C
rew
Oxy
gen
Bot
tle
INTE
RV
AL
NO
TE: C
YLI
ND
ER
SE
RV
ICE
LIF
E (N
ote
1)3A
A-1
800
Unl
imite
d Li
fetim
e (N
ote
2)3H
T-18
50 2
4 Y
ears
(Not
e 3)
Not
e 1:
Cyl
inde
r ser
vice
-life
beg
ins
at th
e in
itial
hyd
rost
atic
test
dat
e of
the
cylin
der.
Not
e 2:
Unl
imite
d lif
etim
e on
con
ditio
n th
at th
e cy
linde
r doe
s no
t fai
l any
re
mai
ning
insp
ectio
n or
hyd
rost
atic
test
requ
irem
ents
.N
ote
3: 2
4 ye
ars
or 4
380
pres
suriz
atio
ns, w
hich
occ
urs
first
.
U29
5
35-0
30-0
135
-30-
00-2
126
GV
I1
A1
A44 46 58
0.04
Vis
ual I
nspe
ctio
n of
the
Por
tabl
e O
xyge
n B
ottle
s fo
r pro
per p
ress
ure
U29
6
35-0
30-0
335
-30-
00-2
118
DE
T24
MO
24 M
O44 46 58
0.05
Det
aile
d In
spec
tion
of th
e P
orta
ble
Oxy
gen
Mas
k&H
ose
Ass
embl
y
U29
7
35-0
30-0
435
-30-
00-9
019
DIS
NO
TEN
OTE
44 46 58
0.30
Dis
card
the
Por
tabl
e O
xyge
n B
ottle
INTE
RV
AL
NO
TE: C
YLI
ND
ER
SE
RV
ICE
LIF
E (N
ote
1)3A
A-1
800
Unl
imite
d Li
fetim
e (N
ote
2)3H
T-18
50 2
4 Y
ears
(Not
e 3)
Not
e 1:
Cyl
inde
r ser
vice
-life
beg
ins
at th
e in
itial
hyd
rost
atic
test
dat
e of
the
cylin
der.
Not
e 2:
Unl
imite
d lif
etim
e on
con
ditio
n th
at th
e cy
linde
r doe
s no
t fai
l any
re
mai
ning
insp
ectio
n or
hyd
rost
atic
test
requ
irem
ents
.N
ote
3: 2
4 ye
ars
or 4
380
pres
suriz
atio
ns, w
hich
occ
urs
first
.
298
ATA
36:
PN
EUM
ATI
C
U29
9
36-0
15-0
136
-10-
04-2
116
DE
T2
C2
C59
5903
A59
04A
0.08
Det
aile
d in
spec
tion
of th
e A
PU
che
ck v
alve
flap
per a
nd h
inge
pin
.
Rev 0 19 March 2014
2-32
MD-80 MAINTENANCE MANUAL
BO
EIN
G P
RO
PR
IETA
RY
- C
opyr
ight
© U
npub
lishe
d W
ork
- See
title
pag
e fo
r det
ails
AU
GU
ST
2013
ME
80-0
20-T
NK
PA
GE
1.1
-25
0 1 2 3 4 5
DC
-9-8
0SF
Mai
nten
ance
Pla
nnin
g D
ocum
ent
SYST
EMS
AN
D P
OW
ERPL
AN
T M
AIN
TEN
AN
CE
PRO
GR
AM
MPD
ITEM
NU
MB
ERAM
M
REF
EREN
CE
C A T
T A S K
INTE
RVA
L
THR
ES.
REP
EAT
TASK
DES
CR
IPTI
ON
ZON
EAC
CES
SM
AN-
HO
UR
S
U30
0
36-0
15-0
236
-10-
03-2
116
DE
T4
C4
C45 51 53 57 59
0.66
Det
aile
d in
spec
tion
of th
e P
neum
atic
man
ifold
isol
atio
n le
ver m
echa
nism
for
cros
sfee
d va
lve
and
cabl
es.
U30
136
-024
-01
36-2
0-02
-710
6O
PC
3 C
3 C
590.
53O
pera
tiona
l che
ck o
f the
tail
com
partm
ent o
verh
eat s
yste
m a
nd a
lerts
.
302
ATA
49:
AIR
BO
RN
E A
UXI
LIA
RY
POW
ER
U30
3
49-0
10-0
149
-10-
05-2
119
DE
TA
PU
CN
GA
PU
CN
G59
5903
A59
04A
0.08
Det
aile
d In
spec
tion
of th
e A
PU
Eng
ine
and
Airf
ram
e M
ount
Ass
embl
y an
d at
tach
ing
hard
war
e.U
304
49-0
30-0
249
-30-
02-9
027
RS
T1
C1
C59
5903
A0.
13C
lean
and
insp
ect t
he A
PU
fuel
con
trol i
nlet
filte
r.
U30
549
-030
-03
49-2
0-00
-210
7G
VI
2 A
2 A
5959
04A
0.07
Gen
eral
Vis
ual I
nspe
ctio
n of
the
AP
U T
urbi
ne P
lenu
m D
rain
.
U30
649
-040
-01
49-4
0-03
-211
7D
ET
1 C
1 C
5959
03A
0.02
Det
aile
d in
spec
tion
of th
e A
PU
sta
rter b
rush
es.
U30
749
-080
-01
49-8
0-01
-210
7G
VI
AP
U C
NG
AP
U C
NG
590.
07G
ener
al v
isua
l ins
pect
ion
of th
e in
side
of t
he A
PU
exh
aust
duc
t.
U30
849
-090
-01
49-9
0-06
-901
9D
IS2
A2
A59
5903
A0.
08C
heck
for c
onta
min
atio
n an
d di
scar
d th
e A
PU
oil
filte
r ele
men
t.
309
ATA
51:
STR
UC
TUR
ES G
ENER
AL
U31
0
51-0
01-0
151
-10-
01-7
10O
PC
1 C
1 C
55 560.
50O
pera
tiona
l Che
ck o
f the
Sla
nt P
ress
ure
Pan
el D
rain
Val
ve
U31
1
51-0
02-0
151
-10-
01-2
80G
VI
4 C
4 C
58N
OTE
0.16
Do
a D
etai
led
Insp
ectio
n of
the
slan
t pre
ssur
e pa
nel d
rain
hol
e, le
ft an
d rig
ht
side
.
AC
CE
SS
NO
TE: R
emov
e pa
ssen
ger s
eats
and
floo
r pan
els
as re
quire
d.
U31
2
51-0
03-0
151
-10-
00-2
11D
ET
24 M
O24
MO
57N
OTE
0.50
Do
a D
etai
led
Insp
ectio
n of
the
Bilg
e D
rain
Val
ves
AC
CE
SS
NO
TE: R
emov
e flo
or p
anel
s as
requ
ired.
313
ATA
52:
DO
OR
S
U31
4
52-0
11-0
112
-21-
01-6
406
LUB
1 C
1 C
46N
OTE
0.25
Lubr
icat
e th
e P
asse
nger
Doo
r Mec
hani
sm
AC
CE
SS
NO
TE: R
emov
e D
oor L
inin
g.
U31
5
52-0
11-0
205
-21-
01-2
116 8
DE
T5
C5
C46
NO
TE0.
67D
etai
led
Insp
ectio
n of
the
Pas
seng
er D
oor a
nd In
terlo
ck M
echa
nism
, Sea
l D
epre
ssor
, Girt
Bar
Lat
ches
, Pre
ssur
e S
eal,
Doo
r Sto
ps a
nd S
et S
crew
s
AC
CE
SS
NO
TE: L
inin
g re
mov
ed.
U31
652
-011
-03
05-2
1-01
-211
6D
ET
1 C
1 C
460.
08D
etai
led
Insp
ectio
n of
the
Pas
seng
er D
oor P
ress
ure
Sea
l
U31
752
-011
-04
52-1
1-00
-720
6FN
C2
C2
C46
0.50
Func
tiona
l Che
ck o
f the
Loc
king
Dev
ice
for t
he D
oor S
et S
crew
s
U31
8
52-0
12-0
112
-21-
01-6
409
LUB
1 C
1 C
58N
OTE
0.25
Lubr
icat
e th
e A
ft C
abin
Bul
khea
d D
oor M
echa
nism
AC
CE
SS
NO
TE: R
emov
e D
oor L
inin
g.
Rev 0 19 March 2014
2-33
MD-80 MAINTENANCE MANUAL
BO
EIN
G P
RO
PR
IETA
RY
- C
opyr
ight
© U
npub
lishe
d W
ork
- See
title
pag
e fo
r det
ails
AU
GU
ST
2013
ME
80-0
20-T
NK
PA
GE
1.1
-26
0 1 2 3 4 5
DC
-9-8
0SF
Mai
nten
ance
Pla
nnin
g D
ocum
ent
SYST
EMS
AN
D P
OW
ERPL
AN
T M
AIN
TEN
AN
CE
PRO
GR
AM
MPD
ITEM
NU
MB
ERAM
M
REF
EREN
CE
C A T
T A S K
INTE
RVA
L
THR
ES.
REP
EAT
TASK
DES
CR
IPTI
ON
ZON
EAC
CES
SM
AN-
HO
UR
S
U31
9
52-0
12-0
205
-21-
01-2
119
DE
T5
C5
C58
NO
TE0.
33D
etai
led
Insp
ectio
n of
the
Aft
Cab
in B
ulkh
ead
Doo
r Mec
hani
sm a
nd s
truct
ure,
D
oor S
eal D
epre
ssor
, Doo
r Sto
ps S
et S
crew
s, a
nd E
mer
genc
y H
andl
e M
echa
nism
AC
CE
SS
NO
TE: R
emov
e do
or li
ning
and
insu
latio
n to
gai
n ac
cess
.
U32
0
52-0
12-0
305
-21-
01-2
119
DE
T1
C1
C58
NO
TE0.
08D
etai
led
Insp
ectio
n of
the
Aft
Cab
in B
ulkh
ead
Doo
r Pre
ssur
e S
eal
AC
CE
SS
NO
TE: L
inin
g re
mov
ed
U32
1
52-0
21-0
112
-21-
01-6
406
LUB
1 C
1 C
58N
OTE
0.80
Lubr
icat
e th
e O
verw
ing
Em
erge
ncy
Exi
t Doo
r Mec
hani
sm
AC
CE
SS
NO
TE: R
emov
e do
or li
ning
.
U32
2
52-0
21-0
205
-21-
01-2
116
DE
T5
C5
C58
NO
TE1.
33D
etai
led
Insp
ectio
n of
the
Ove
rwin
g E
mer
genc
y E
xit D
oor M
echa
nism
, Pre
ssur
e S
eal D
epre
ssor
, Doo
r Sto
ps a
nd S
et S
crew
s an
d Lo
ck P
in S
ocke
t Ass
embl
y
AC
CE
SS
NO
TE: R
emov
e Li
ning
.
U32
3
52-0
21-0
305
-21-
01-2
116
DE
T1
C1
C58
NO
TE0.
26D
etai
led
Insp
ectio
n of
the
Ove
rwin
g E
mer
genc
y E
xit D
oor P
ress
ure
Sea
l
AC
CE
SS
NO
TE: R
emov
e E
mer
genc
y E
xit D
oors
.
U32
4
52-0
21-0
452
-21-
00-7
106
OP
C2
C2
C58
1.00
Ope
ratio
nal C
heck
of t
he O
verw
ing
Em
erge
ncy
Exi
t Doo
r Pre
ssur
e S
eal
Mec
hani
sm
U32
5
52-0
30-0
112
-21-
01-6
406
LUB
1 C
1 C
51 57N
OTE
0.75
Lubr
icat
e th
e C
argo
Doo
r Mec
hani
sm
AC
CE
SS
NO
TE: R
emov
e th
e ap
plic
able
acc
ess
cove
r.
U32
6
52-0
30-0
205
-21-
01-2
116 9
DE
T5
C5
C51 57
NO
TE1.
00D
etai
led
Insp
ectio
n of
the
Car
go D
oor M
echa
nism
, Car
go B
arrie
r, H
old
Ope
n M
echa
nism
, Sto
ps a
nd S
et S
crew
s
AC
CE
SS
NO
TE: R
emov
e ca
rgo
door
lini
ng a
nd in
sula
tion.
U32
7
52-0
30-0
305
-21-
01-2
116
DE
T1
C1
C51 57
0.25
Det
aile
d In
spec
tion
of th
e C
argo
Doo
r Pre
ssur
e S
eal
U32
8
52-0
30-0
452
-31-
00-7
206
FNC
2 C
2 C
51 570.
75Fu
nctio
nal C
heck
of t
he L
ocki
ng D
evic
e fo
r the
Car
go D
oor S
et S
crew
s
U32
9
52-0
41-0
105
-21-
01-2
116
DE
T5
C5
C45
NO
TE0.
33D
etai
led
Insp
ectio
n of
the
Avi
onic
s C
ompa
rtmen
t Doo
r Mec
hani
sm, S
eal
Dep
ress
or, A
vion
ics
Com
partm
ent D
oor S
tops
and
Set
Scr
ews
AC
CE
SS
NO
TE: L
inin
g re
mov
ed.
U33
0
52-0
41-0
205
-21-
01-2
116
DE
T1
C1
C43 45
0.17
Det
aile
d In
spec
tion
of th
e A
vion
ics
and
Forw
ard
Acc
esso
ry C
ompa
rtmen
t Doo
r S
eals
U33
1
52-0
41-0
352
-43-
00-7
206
FNC
2 C
2 C
450.
08Fu
nctio
nal C
heck
of t
he L
ocki
ng D
evic
e fo
r the
Avi
onic
s C
ompa
rtmen
t Doo
r Set
S
crew
s
Rev 0 19 March 2014
2-34
MD-80 MAINTENANCE MANUAL
BO
EIN
G P
RO
PR
IETA
RY
- C
opyr
ight
© U
npub
lishe
d W
ork
- See
title
pag
e fo
r det
ails
AU
GU
ST
2013
ME
80-0
20-T
NK
PA
GE
1.1
-27
0 1 2 3 4 5
DC
-9-8
0SF
Mai
nten
ance
Pla
nnin
g D
ocum
ent
SYST
EMS
AN
D P
OW
ERPL
AN
T M
AIN
TEN
AN
CE
PRO
GR
AM
MPD
ITEM
NU
MB
ERAM
M
REF
EREN
CE
C A T
T A S K
INTE
RVA
L
THR
ES.
REP
EAT
TASK
DES
CR
IPTI
ON
ZON
EAC
CES
SM
AN-
HO
UR
S
U33
2
52-0
42-0
112
-21-
01-6
406
LUB
1 C
1 C
46N
OTE
0.25
Lubr
icat
e th
e Fo
rwar
d G
alle
y S
ervi
ce D
oor M
echa
nism
AC
CE
SS
NO
TE: R
emov
e lin
ing.
U33
3
52-0
42-0
205
-21-
01-2
116 8
DE
T5
C5
C46
NO
TE0.
33D
etai
led
Insp
ectio
n of
the
Forw
ard
Gal
ley
Ser
vice
Doo
r Mec
hani
sm, S
eal
Dep
ress
or, G
irt B
ar L
atch
es, D
oor S
tops
and
Set
Scr
ews
AC
CE
SS
NO
TE: L
inin
g re
mov
ed.
U33
452
-042
-03
05-2
1-01
-211
6D
ET
1 C
1 C
460.
08D
etai
led
Insp
ectio
n of
the
Forw
ard
Gal
ley
Ser
vice
Doo
r Sea
l
U33
5
52-0
42-0
452
-41-
00-7
206
FNC
2 C
2 C
460.
50Fu
nctio
nal C
heck
of t
he L
ocki
ng D
evic
e fo
r the
For
war
d G
alle
y S
ervi
ce D
oor S
et
Scr
ews
U33
6
52-0
43-0
112
-21-
01-6
406
LUB
1 C
1 C
58N
OTE
0.25
Lubr
icat
e th
e A
ft G
alle
y S
ervi
ce D
oor M
echa
nism
AC
CE
SS
NO
TE: L
inin
g re
mov
ed.
U33
7
52-0
43-0
205
-21-
01-2
116 8
DE
T5
C5
C58
NO
TE0.
33D
etai
led
Insp
ectio
n of
the
Aft
Gal
ley
Ser
vice
Doo
r Mec
hani
sm, S
eal D
epre
ssor
, G
irt B
ar L
atch
es, D
oor S
tops
and
Set
Scr
ews
AC
CE
SS
NO
TE: L
inin
g re
mov
ed.
U33
852
-043
-03
05-2
1-01
-211
6D
ET
1 C
1 C
580.
08D
etai
led
Insp
ectio
n of
the
Aft
Gal
ley
Ser
vice
Doo
r Sea
l
U33
9
52-0
43-0
452
-42-
00-7
206
FNC
2 C
2 C
580.
50Fu
nctio
nal C
heck
of t
he L
ocki
ng D
evic
e fo
r the
Aft
Gal
ley
Ser
vice
Doo
r Set
S
crew
s
AIR
PLA
NE
NO
TE: A
pplic
able
to fu
sela
ge p
rior t
o 14
12 th
at h
ave
not
inco
rpor
ated
Ser
vice
Bul
letin
52-
161.
U34
0
52-0
45-0
152
-45-
00-7
209
FNC
4 C
4 C
590.
08Fu
nctio
nal C
heck
of t
he A
PU
Com
partm
ent D
oor P
ress
ure
Rel
ief D
oor L
atch
es
U34
1
52-0
45-0
205
-21-
01-2
118
DE
T4
C4
C61
5903
A59
04A
0.08
Det
aile
d In
spec
tion
of th
e A
PU
Doo
r Hin
ges
and
Cam
lock
Fas
tene
r
U34
252
-054
-01
52-5
2-01
-720
8FN
C2
C2
C44
0.05
Func
tiona
l Che
ck o
f the
Flig
ht C
ompa
rtmen
t Doo
r Blo
wou
t Pan
els
U34
3
52-0
61-0
112
-21-
01-6
406
LUB
1 C
1 C
45N
OTE
0.08
Lubr
icat
e th
e M
ain
Ent
ranc
e S
tairw
ay a
nd D
oor m
echa
nism
AC
CE
SS
NO
TE: F
orw
ard
Ent
ry S
tairs
Ext
ende
d.
U34
4
52-0
61-0
205
-21-
01-2
116
DE
T2
C2
C45
0.16
Det
aile
d In
spec
tion
of th
e M
ain
Ent
ranc
e S
tairw
ay D
oor L
atch
ing
mec
hani
sm
U34
5
52-0
61-0
405
-21-
01-2
116
DE
T1
C1
C45
NO
TE0.
08D
etai
led
Insp
ectio
n of
the
Mai
n E
ntra
nce
Sta
irway
Doo
r Sea
l
AC
CE
SS
NO
TE: F
orw
ard
Ent
ry S
tairs
Ext
ende
d.
U34
6
52-0
62-0
112
-21-
01-6
406
LUB
1 C
1 C
59N
OTE
0.08
Lubr
icat
e th
e A
ft E
ntry
Sta
irway
mec
hani
sm
AC
CE
SS
NO
TE: L
ower
Aft
Ent
ry S
tairs
.
Rev 0 19 March 2014
2-35
MD-80 MAINTENANCE MANUAL
BO
EIN
G P
RO
PR
IETA
RY
- C
opyr
ight
© U
npub
lishe
d W
ork
- See
title
pag
e fo
r det
ails
AU
GU
ST
2013
ME
80-0
20-T
NK
PA
GE
1.1
-28
0 1 2 3 4 5
DC
-9-8
0SF
Mai
nten
ance
Pla
nnin
g D
ocum
ent
SYST
EMS
AN
D P
OW
ERPL
AN
T M
AIN
TEN
AN
CE
PRO
GR
AM
MPD
ITEM
NU
MB
ERAM
M
REF
EREN
CE
C A T
T A S K
INTE
RVA
L
THR
ES.
REP
EAT
TASK
DES
CR
IPTI
ON
ZON
EAC
CES
SM
AN-
HO
UR
S
U34
7
52-0
62-0
212
-21-
01-6
406
LUB
2 C
2 C
61N
OTE
0.05
Lubr
icat
e th
e A
ft E
ntry
Sta
irway
Doo
r Mec
hani
sm C
ontro
l Cab
les
AC
CE
SS
NO
TE: L
ower
Aft
Ent
ry S
tairs
.
U34
8
52-0
62-0
352
-63-
00-2
116
DE
T4
C4
C61
0.16
Det
aile
d In
spec
tion
of th
e A
ft E
ntry
Sta
irway
Doo
r Mec
hani
sm C
ontro
l Cab
les
U34
9
52-0
70-0
152
-70-
00-7
109
OP
C1
C1
C42 44 45 46 51 57 58 61
0.18
Ope
ratio
nal C
heck
of t
he D
oor W
arni
ng S
yste
m
350
ATA
56:
WIN
DO
WS
U35
156
-011
-01
56-1
0-01
-211
6D
ET
2 C
2 C
440.
50D
etai
led
insp
ectio
n of
the
left,
cen
ter a
nd ri
ght w
inds
hiel
d.
U35
256
-012
-01
56-1
0-03
-710
9O
PC
2 C
2 C
440.
18O
pera
tiona
l Che
ck o
f the
Slid
ing
Cle
arvi
ew W
indo
w
U35
356
-012
-02
12-2
1-03
-640
9LU
B1
C1
C44
0.08
Lubr
icat
e th
e S
lidin
g C
lear
view
Win
dow
Ass
embl
y
U35
456
-012
-03
05-2
1-01
-211
6D
ET
2 C
2 C
440.
08D
etai
led
Insp
ectio
n of
the
Cle
arvi
ew W
indo
w P
ress
ure
Sea
l
U35
5
56-0
21-0
156
-20-
00-2
118
DE
T8
C8
C40 50
8.50
Det
aile
d In
spec
tion
of th
e C
abin
and
Doo
r Win
dow
Pan
es
AIR
PLA
NE
NO
TE: I
nspe
ctio
n of
win
dow
pan
e ed
ges
is w
ith a
pris
m s
o th
e pa
ne
does
n't h
ave
to b
e re
mov
ed.
356
ATA
57:
WIN
GS
U35
7
57-0
02-0
012
-21-
02-6
40LU
B1
C1
C15 16
0.50
Do
a lu
bric
atio
n of
the
artic
ulat
ed b
ent-u
p tra
iling
edge
(BU
TE) d
oors
and
ro
llers
.
U35
8
57-0
03-0
057
-20-
03-2
11D
ET
1 C
1 C
15 162.
00D
o a
deta
iled
insp
ectio
n of
the
left
and
right
win
g bu
te d
oor r
olle
rs a
nd h
inge
for
wea
r and
con
ditio
n.
359
ATA
71:
PO
WER
PLA
NT
U36
0
71-0
10-0
171
-10-
01-2
116
DE
T1
C1
C73 74
7303
C73
05C
7306
C73
07C
7309
C74
02C
7403
C74
04C
7406
C74
08C
0.20
Det
aile
d In
spec
tion
of th
e in
tern
al N
ose
Cow
l and
atta
chm
ents
Rev 0 19 March 2014
2-36
MD-80 MAINTENANCE MANUAL
BO
EIN
G P
RO
PR
IETA
RY
- C
opyr
ight
© U
npub
lishe
d W
ork
- See
title
pag
e fo
r det
ails
AU
GU
ST
2013
ME
80-0
20-T
NK
PA
GE
1.1
-29
0 1 2 3 4 5
DC
-9-8
0SF
Mai
nten
ance
Pla
nnin
g D
ocum
ent
SYST
EMS
AN
D P
OW
ERPL
AN
T M
AIN
TEN
AN
CE
PRO
GR
AM
MPD
ITEM
NU
MB
ERAM
M
REF
EREN
CE
C A T
T A S K
INTE
RVA
L
THR
ES.
REP
EAT
TASK
DES
CR
IPTI
ON
ZON
EAC
CES
SM
AN-
HO
UR
S
U36
1
71-0
10-0
571
-10-
03-2
119
DE
T1
C1
C71 72
0.27
Det
aile
d In
spec
tion
of th
e in
ner s
urfa
ces
of th
e C
owl D
oors
and
sea
ls
U36
2
71-0
10-0
671
-10-
04-2
119
DE
TE
NG
CN
GE
NG
CN
G71 72
0.33
Det
aile
d In
spec
tion
of th
e U
nder
cow
l Pyl
on A
pron
sur
face
U36
3
71-0
10-1
071
-10-
03-2
119
DE
T1
C1
C71 72
0.13
Det
aile
d In
spec
tion
of th
e E
ngin
e C
owl G
roun
d S
afet
y La
tch
U36
4
71-0
10-1
171
-10-
03-2
119
DE
T1
C1
C71 72
0.17
Det
aile
d In
spec
tion
of th
e Fa
n C
owl H
old
Ope
n R
od S
tora
ge a
nd a
ttach
men
ts
U36
5
71-0
10-1
271
-10-
03-2
119
DE
T1
C1
C71 72
0.08
Det
aile
d In
spec
tion
of th
e S
nubb
er R
eel a
nd a
ttach
men
ts
U36
6
71-0
10-1
371
-10-
03-2
119
DE
T1
C1
C71 72
0.17
Det
aile
d In
spec
tion
of th
e Fa
n C
owl H
inge
/Bea
ms
U36
7
71-0
10-1
471
-10-
03-2
119
DE
T1
C1
C71 72
0.17
Det
aile
d In
spec
tion
of th
e Fa
n C
owl L
atch
es a
nd a
ttach
ing
hard
war
e an
d at
tach
men
ts
U36
8
71-0
10-1
571
-10-
01-7
20FN
C72
MO
72 M
O73 74
0.10
Func
tiona
l Che
ck o
f the
Eng
ine
Nos
e C
owl O
ver T
empe
ratu
re In
dica
tor
U36
9
71-0
10-1
671
-10-
01-2
806
SD
I10
00 F
H50
00 F
H73 74
7303
C73
05C
7306
C73
07C
7309
C74
02C
7403
C74
04C
7406
C74
08C
0.84
Spe
cial
Det
aile
d In
spec
tion
(tap
test
) of t
he E
ngin
e N
ose
Cow
l Inn
er B
arre
l A
cous
tic P
anel
Ski
n to
Cor
e A
ttach
men
t.
U37
0
71-0
20-0
171
-20-
01-2
409
SD
IE
NG
CN
GE
NG
CN
G71 72
0.50
Spe
cial
Det
aile
d In
spec
tion
of th
e E
ngin
e M
ount
Con
e B
olts
U37
1
71-0
20-0
271
-20-
02-2
119
DE
T1
CE
NG
CN
GN
OTE
1 C
EN
G C
NG
NO
TE
81 820.
33D
etai
led
Insp
ectio
n of
the
Eng
ine
Mou
nt V
ibra
tion
Isol
ator
s
INTE
RV
AL
NO
TE: W
hich
ever
occ
urs
first
U37
2
71-0
20-0
412
-21-
05-6
408
LUB
120
MO
72 M
O81 82
0.33
Lubr
icat
ion
of th
e E
ngin
e M
ount
Fro
nt Y
oke
Bol
ts
U37
3
71-0
30-0
105
-21-
01-2
108
GV
I1
C1
C71 72
NO
TE0.
16G
ener
al V
isua
l Ins
pect
ion
of th
e E
ngin
e B
urn-
Thru
Bar
rier.
AC
CE
SS
NO
TE: O
pen
engi
ne n
acel
le d
oors
.
U37
4
71-0
71-0
271
-70-
01-7
109
OP
C1
C1
C71 72
0.20
Ope
ratio
nal C
heck
of t
he P
ower
plan
t Dra
in L
ines
and
Dra
in M
ast
375
ATA
72:
EN
GIN
E
Rev 0 19 March 2014
2-37
MD-80 MAINTENANCE MANUAL
BO
EIN
G P
RO
PR
IETA
RY
- C
opyr
ight
© U
npub
lishe
d W
ork
- See
title
pag
e fo
r det
ails
AU
GU
ST
2013
ME
80-0
20-T
NK
PA
GE
1.1
-30
0 1 2 3 4 5
DC
-9-8
0SF
Mai
nten
ance
Pla
nnin
g D
ocum
ent
SYST
EMS
AN
D P
OW
ERPL
AN
T M
AIN
TEN
AN
CE
PRO
GR
AM
MPD
ITEM
NU
MB
ERAM
M
REF
EREN
CE
C A T
T A S K
INTE
RVA
L
THR
ES.
REP
EAT
TASK
DES
CR
IPTI
ON
ZON
EAC
CES
SM
AN-
HO
UR
S
U37
6
72-0
20-0
172
-21-
00-2
116
DE
T1
C1
C71 72
0.20
Det
aile
d In
spec
tion
of th
e Fr
ont A
cces
sory
Sup
port
Ass
embl
y
U37
7
72-0
30-0
172
-36-
00-2
906 7
SD
I1
C1
C71 72
3.00
Spe
cial
Det
aile
d In
spec
tion
of th
e 13
th c
ompr
esso
r bla
des
Aft
Face
(B
ores
cope
)
U37
8
72-0
30-0
372
-33-
00-2
116
DE
T1
A1
A71 72
0.20
Det
aile
d In
spec
tion
of th
e vi
sibl
e pa
rts o
f the
fan
blad
es
U37
9
72-0
30-0
472
-33-
02-9
016
DIS
NO
TEN
OTE
71 720.
01D
isca
rd th
e C
ompr
esso
r Rot
or
INTE
RV
AL
NO
TE: A
ll en
gine
com
pone
nts
safe
life
lim
its w
ill be
mai
ntai
ned
per
JT8D
Eng
ine
Man
ual (
PN
773
128)
, #05
-10-
01, T
ime
Lim
its.
U38
0
72-0
50-0
172
-52-
00-2
906 9
SD
I1
C1
C71 72
0.76
Spe
cial
Det
aile
d In
spec
tion
of th
e Fo
rwar
d Fa
ce o
f the
1S
T S
tage
Tur
bine
V
anes
and
Tur
bine
Bla
des
(Bor
esco
pe)
U38
1
72-0
50-0
272
-52-
00-9
015
DIS
NO
TEN
OTE
71 720.
01D
isca
rd th
e Tu
rbin
e D
isks
INTE
RV
AL
NO
TE: A
ll en
gine
com
pone
nts
safe
life
lim
its w
ill be
mai
ntai
ned
per
JT8D
Eng
ine
Man
ual (
PN
773
128)
, #05
-10-
01,T
ime
Lim
its
U38
2
72-0
50-0
372
-53-
00-2
116
DE
T1
C1
C71 72
1.00
Det
aile
d In
spec
tion
of th
e 4T
H S
tage
Tur
bine
Bla
des,
Van
es, a
nd O
uter
Air
Sea
l (V
iew
ed fr
om E
xhau
st)
U38
3
72-0
60-0
172
-61-
00-2
116
GV
I1
C1
C71 72
0.01
Insp
ect M
agne
tic C
hip
Det
ecto
r
384
ATA
73:
EN
GIN
E FU
EL A
ND
CO
NTR
OL
U38
5
73-0
01-0
273
-12-
01-9
016
DIS
1 C
1 C
71 720.
16In
spec
t for
con
tam
inat
ion
and
disc
ard
the
Mai
n Fu
el F
ilter
386
ATA
74:
IGN
ITIO
N
U38
7
74-0
01-0
174
-20-
02-9
016
DIS
1 C
1 C
71 7259
01C
5902
C0.
06D
isca
rd th
e Ig
nite
r Plu
gs
388
ATA
76:
EN
GIN
E C
ON
TRO
LS
U38
9
76-0
11-0
120
-10-
17-2
116
DE
T4
C4
C45 51 53 57
NO
TE0.
68D
etai
led
Insp
ectio
n of
the
left
and
right
thro
ttle
cabl
e sy
stem
(Une
xpos
ed A
rea)
AC
CE
SS
NO
TE: O
pen
ceilin
g pa
nels
in F
WD
and
AFT
car
go c
ompa
rtmen
ts,
and
rem
ove
floor
pan
els
and
seat
s as
requ
ired
over
cen
ter w
ing
sect
ion
to
faci
litat
e m
aint
enan
ce.
U39
076
-011
-02
76-1
1-02
-901
RS
T50
00 F
H50
00 F
H71
1.00
Res
tora
tion
of th
e E
ngin
e S
ynch
roni
zer R
od E
nd T
rimm
er A
ssem
bly
Rev 0 19 March 2014
2-38
MD-80 MAINTENANCE MANUAL
BO
EIN
G P
RO
PR
IETA
RY
- C
opyr
ight
© U
npub
lishe
d W
ork
- See
title
pag
e fo
r det
ails
AU
GU
ST
2013
ME
80-0
20-T
NK
PA
GE
1.1
-31
0 1 2 3 4 5
DC
-9-8
0SF
Mai
nten
ance
Pla
nnin
g D
ocum
ent
SYST
EMS
AN
D P
OW
ERPL
AN
T M
AIN
TEN
AN
CE
PRO
GR
AM
MPD
ITEM
NU
MB
ERAM
M
REF
EREN
CE
C A T
T A S K
INTE
RVA
L
THR
ES.
REP
EAT
TASK
DES
CR
IPTI
ON
ZON
EAC
CES
SM
AN-
HO
UR
S
U39
1
76-0
13-0
120
-10-
17-2
116
DE
T4
C4
C45 51 53 57
NO
TE0.
83D
etai
led
Insp
ectio
n of
the
fuel
shu
toff
leve
r cab
le s
yste
m (U
nexp
osed
Are
a)
AC
CE
SS
NO
TE: O
pen
ceilin
g pa
nels
in F
WD
and
AFT
car
go c
ompa
rtmen
ts,
and
rem
ove
floor
pan
els
and
seat
s as
requ
ired
over
cen
ter w
ing
sect
ion
to
faci
litat
e m
aint
enan
ce.
U39
2
76-0
21-0
176
-20-
00-7
108
OP
CE
NG
CN
GE
NG
CN
G44 55 56 59
0.23
Ope
ratio
nal C
heck
of t
he E
ngin
e E
mer
genc
y S
hutd
own
Sys
tem
U39
3
76-0
21-0
276
-20-
00-2
118
DE
T4
C4
C15 16 45 51 53 55 56 57 59
2.50
Det
aile
d In
spec
tion
of th
e E
ngin
e E
mer
genc
y S
hutd
own
Sys
tem
Cab
les
(Une
xpos
ed A
rea)
394
ATA
78:
EXH
AU
ST
U39
5
78-0
30-0
278
-31-
01-7
206
FNC
4 C
4 C
5959
01C
5902
C0.
27Fu
nctio
nal C
heck
of t
he T
hrus
t Rev
erse
r Sys
tem
to h
old
pres
sure
with
out M
ain
Hyd
raul
ic P
ress
ure
U39
6
78-0
30-0
378
-32-
01-7
209
FNC
1 C
1 C
5959
01C
5902
C0.
20Fu
nctio
nal C
heck
of t
he T
hrus
t Rev
erse
r Sys
tem
Low
Pre
ssur
e W
arni
ng S
witc
h
397
ATA
79:
OIL
U39
8
79-0
01-0
279
-20-
06-9
026
RS
T1
A1
A71 72
5901
C59
02C
0.17
Cle
an o
r Rep
lace
Mai
n E
ngin
e O
il Fi
lter a
nd c
heck
for c
onta
min
atio
n.
U39
9
79-0
30-0
179
-35-
01-7
209
FNC
2 C
2 C
71 720.
67Fu
nctio
nal C
heck
of t
he E
ngin
e O
il S
train
er In
dica
tion
Sys
tem
400
ATA
80:
STA
RTI
NG
U40
1
80-0
01-0
112
-12-
05-2
126
GV
I2
A2
A71 72
0.02
Che
ck S
tarte
r Oil
U40
2
80-0
01-0
280
-10-
02-1
106
RS
T1
C1
C71 72
5901
C59
02C
0.07
Res
tore
the
Sta
rter S
/O V
alve
Inlin
e Fi
lter
U40
3
80-0
01-0
380
-10-
01-6
10S
VC
2 A
2 A
71 720.
50S
ervi
ce L
eft a
nd R
ight
Eng
ine
Sta
rter O
il
Rev 0 19 March 2014
3-1
MD-80 MAINTENANCE MANUAL
CHAPTER 3: STRUCTURAL MAINTENANCE PROGRAM
3.1 Scope
This chapter of the MPD outlines the scheduled maintenance tasks for the Structural Maintenance Pro-gram. This program is designed to provide timely detection and repair of structural damage which may occur in the fleet during commercial operations. Detection of corrosion, stress corrosion, minor accidental damage and fatigue cracking by visual and/or Non-Destructive Test (NDT) procedures is considered. Major accidental damage such as that caused by bird strike or large ground handling equipment is consid-ered readily detectable. Additionally, tell-tale signs such as fuel leaks, loose fasteners, loss of cabin pres-sure, etc. are considered readily detectable and continue to be an essential part of the Structural Maintenance Program.
This baseline program is intended to serve as a guide for airlines to develop individual maintenance pro-grams. The tasks listed herein constitute the initial minimum requirements and manufacturer’s recommen-dations for all MD-80 airplanes. Operators are cautioned that time extensions for their fleet should be based on service bulletin status as well as service experience.
Notes applicable to the Structural Maintenance Program are followed by explanations of the operating rules, fatigue related inspection program, corrosion prevention and control program, reporting of structural maintenance tasks, and the page format.
3.2 Notes: Main Cargo Door Modification (STC ST02434LA)
1. Scheduled maintenance tasks for the main cargo door modification can be found in Chapter 12.
3.3 Notes
1. Tasks for detecting corrosion, stress corrosion, minor accidental damage and fatigue damage using visual and/or Non-Destructive Test (NDT) procedures are specified. After discrepancies are found, repair or modification action may be required to assure continuing airworthiness of the airplane.
2. Inspection
An examination of an item against a specific standard to detect irregularities and discrepancies such as wear, deterioration, damage, corrosion, cracking, etc.
3.3.1 Inspection Task Definitions
3.3.1.1 Inspection - General Visual
A visual examination of an interior or exterior area, installation or assembly to detect obvious damage, fail-ure or irregularity. This level of inspection is made from within touching distance, unless otherwise speci-fied. A mirror may be necessary to enhance visual access to all exposed surfaces in the inspection area. This level of inspection is made under normally available lighting conditions such as daylight, hangar lighting, flashlight or drop-light and may require removal or opening of access panels or doors. Stands, ladders or platforms may be required to gain proximity to the area being checked.
3.3.1.2 Inspection - Detailed
An intensive visual examination of a specific structural area, system, installation or assembly to detect damage, failure or irregularity. Available lighting is normally supplemented with a direct source of good lighting at an intensity deemed appropriate by the inspector. Inspection aids such as mirrors, magnifying lenses, etc. may be used. Surface cleaning and elaborate access procedures may be required.
Rev 0 19 March 2014
3-2
MD-80 MAINTENANCE MANUAL
3.3.1.3 Inspection - Special Detailed
An intensive examination of a specific item(s), installation or assembly to detect damage, failure or irregu-larity. The examination is likely to make extensive use of specialized inspection techniques and/or equip-ment. Intricate cleaning and substantial access or disassembly procedures may be required.
3.4 Operating Rules
1. All airplanes in an operator’s or group of operators’ fleet shall be subject to the provisions of this chap-ter. These include requirements for external and internal structural inspections, corrosion prevention and control tasks, and fatigue related inspections.
2. Intervals for the structural maintenance program are expressed in calendar time and/or flight cycles. Any interval change would be substantiated by service experience and handled by FAA approved pro-gram revision procedures as applicable to each operator or group of operators.
3. Supplemental Inspection Document (DM-IS-SID-80) provides specifics on Principle Structural Ele-ments (PSE) inspections.
4. Special Detailed Inspections are to be used when specified for inspecting hidden details or may be used as alternatives to detailed visual inspections. Hidden details requiring NDT procedures are listed under appropriate zones either internally or externally. Procedures for conducting these Special Detailed Inspections are given in the Boeing Non-Destructive Test Standard Practices Manual (MDC-93K0393).
5. Normal cleanup procedures are to be used prior to conducting general visual or detailed inspections. Specified cleanup procedures are to be used for special detailed inspections. Sealant and corrosion pro-tection finishes should only be removed when specified and restored in accordance with the Corrosion Control Handbook (CCH) - MDC K0805 after the task is completed.
6. Excessive dust, debris, or overspray of corrosion inhibiting compounds, found during any inspection, are considered to be unsatisfactory condition possibly reducing the fire resistance of the airplane design. Cleanup of these materials should be a standard part of maintenance activity.
3.5 Fatigue Related Inspection Program
Where the initial scheduled maintenance program does not ensure timely detection of potential fatigue damage in a structural item, supplemental fatigue related inspections will be required for all of the MD-80 fleet. Such supplemental inspections will begin after the threshold defined in the MD-80 Supplemental Inspection Document (SID) is reached and must be accomplished within one repeat interval of the thresh-old.
One feasible supplemental inspection program has been developed for all affected structure. The resulting inspections are identified by the letter “F” (For Fatigue) in the program (PGM) column. These inspections must be accomplished prior to reaching the fatigue task threshold. All fatigue task threshold intervals vary and are included in the MD-80 Supplemental Inspection Document. In addition, they are based on the ini-tial structures task interval. Escalation of the initial and repeat MD-80 Supplemental Inspection Document intervals is not permitted.
3.6 Corrosion Prevention and Control Requirements
The MD-80 MSG-3 Maintenance Review Board (MRB) Report, Structures Program is an FAA Approved equivalent program to the MD-80 CPCP document MDCK4606 as mandated in AD 92-22-08R1. There-fore, the structures tasks in the MD-80 MSG-3 MRB Report are not controlled by AD 92-22-08R1. AD 92-22-08R1 is only applicable to airplanes that are maintained in accordance with MD-80 CPCP document MDC-K4606.
Rev 0 19 March 2014
3-3
MD-80 MAINTENANCE MANUAL
3.7 Corrosion Prevention and Control Program
Structural maintenance requirements are determined on the basis of continual maintenance to preserve or restore the inherent corrosion preventive measures and structural surface finishes. Should corrosion be detected or should the corrosion inhibiting compound exhibit signs of deterioration during the performance of a structural task, the Corrosion Control Handbook (CCH) - MDC K0805 should be referred to for appro-priate corrective action. The CCH provides general information on inspection, detection, and removal of corrosion as well as preventive maintenance practices for corrosion control. Tasks in which periodic appli-cation of corrosion inhibiting compounds are recommended or required are contained in this chapter.
The Corrosion Prevention and Control Program (CPCP) is an integral part of the Structural Maintenance Program. The objective of the CPCP is to control corrosion found on all structure listed in the Structural Maintenance Program to Level 1 or better.
To reiterate, the Corrosion Prevention and Control Program (CPCP) is an integral part of the Structural Maintenance Program. The objective of the CPCP is to control corrosion found on all structure listed in the Structural Maintenance Program to Level 1 or better. Refer to section 1 for the CPCP basic task.
The CPCP basic task consists of the following items:
1. Remove all systems, equipment and interior furnishings, etc. (e.g. toilets, galleys, lining, insulation) as necessary to accomplish item 3. It is not necessary to remove bushings unless specified in the task description, or if there is an indication of corrosion, or that the bushing has migrated.
2. Prior to inspection, clean the area as necessary to accomplish item 3. It is not necessary to remove nor-mal amounts of sealant/leveling compound unless it has deteriorated to the point where moisture can penetrate down to the metal. A light uniform film of corrosion inhibiting compound (CIC) that has not accumulated dirt or debris will normally allow adequate inspection of the structure without removal. CIC may require removal if there are multiple layers and/or accumulations of dirt or debris.
3. Visually inspect all structure listed in the Structural Maintenance Program. The inspection method is as specified in each task description. Use additional non-destructive inspections or visual inspections following partial disassembly if there are indications of hidden corrosion, such as bulging skins, or corrosion running into splices, or under fittings, etc. In the task area, check the integrity of any sealant/leveling compound to determine if removal is required, and check corrosion inhibiting compound, par-ticularly at faying surfaces, to determine if additional application is required per item 6.
4. Remove all corrosion, evaluate damage, and repair or replace all discrepant structure as necessary, including restoration of protective finishes.
5. Clear any blocked holes or gaps that may hinder drainage, as applicable.
6. Apply suitable approved water-displacing/anti-corrosion compounds, as necessary.
NOTE: Optional procedures for applying these compounds are given in the Boeing CCH (MDC K0805).
a. The minimum requirement for all areas (except as noted in 6c) is a single coat of water displacing/anti-corrosion compound that penetrates faying surfaces and displaces moisture, where the initial or previous coat has been disturbed or removed.
b. In areas with high potential for severe corrosion, where the initial or previous coat has been dis-turbed or removed, the application of water displacing/anti-corrosion compound(s) that penetrates faying surfaces, displaces moisture and forms a durable barrier after drying is recommended (but optional). This can be achieved by applying a single coat per Boeing CCH (MDC K0805).
c. Water displacing/anti-corrosion compounds should not be applied in the following areas:
i. Cables, pulleys, wiring, plastics, elastomers, oxygen systems.
ii. Lubricated or teflon surfaces (e.g. greased joints, sealed bearings).
iii. Adjacent to tears or holes in insulation blankets.
Rev 0 19 March 2014
3-4
MD-80 MAINTENANCE MANUAL
iv. Areas with electrical arc potential.
v. Interior materials, including cargo liners.
vi. Engine strut cavities, cowling panels or pod.
vii. APU or any structure in direct contact with the APU.
viii.Fiberglass ducts where temperature exceeds 220 degrees Fahrenheit.
7. Dry any wet insulation blankets prior to re-installing, or replace with new, as applicable.
3.8 Corrosion Level Definition
3.8.1 Corrosion Level 1
Corrosion occurring between successive inspections that is local and can be reworked/blended-out within manufacturer’s allowable limits (e.g., SRM, Service Bulletin, etc.).
or
Corrosion occurring between successive inspections exceeds allowable limit but is local and can be attrib-uted to an event not typical of operator usage of other aircraft in the same fleet (e.g., mercury spill).
or
Operator experience over several inspections has demonstrated only light corrosion between each sched-uled inspection but the latest inspection and cumulative blend-out now exceeds allowable limits. The terms “local corrosion” and “light corrosion” are model specific and will be determined by the manufacturer and published in appropriate maintenance documents.
3.8.2 Corrosion Level 2
Corrosion occurring between successive inspections that requires a single re-work / blend- out which then exceeds allowable limits, requiring a repair / reinforcement, or complete or partial replacement of structure listed in the Baseline Program or, Corrosion occurring between successive inspections that is widespread and requires a single blend-out approaching allowable rework limits.
3.8.3 Corrosion Level 3
Corrosion found during the first or subsequent inspections, which is determined (normally by the operator) to be an urgent airworthiness concern, requiring expeditious action.
NOTE: When LEVEL 3 corrosion is found, consideration should be given to action required on other airplanes in the operator's fleet. Details of the corrosion finding and planned action(s) should be expeditiously reported to the appropriate regulatory authority.
AN EFFECTIVE PROGRAM IS ONE THAT CONTROLS CORROSION OF ALL STRUCTURE LISTED IN THE BASELINE PROGRAM TO LEVEL 1 OR BETTER.
Level 2 corrosion findings in an area require a program adjustment to reduce damage to Level 1 or better.
Level 3 findings require timely inspections to verify the structural integrity of the remaining aircraft in the operator’s fleet.
3.9 Reporting Results of Structural Inspections
Reports of structural significant defects, as defined by the 14 CFR § 121.703 – Service Difficulty Reports (SDR), shall be submitted to the administrator, by operators operating under FAA regulations.
Rev 0 19 March 2014
3-5
MD-80 MAINTENANCE MANUAL
Figure 3-A: Structures Maintenance Program Example Page
Rev 0 19 March 2014
3-6
MD-80 MAINTENANCE MANUAL
3.10 Page Format Explanation
1. MPD Item Number.
Each task is given a unique MPD item number. The first and second digit is the ATA number. The rest of the numbers denote the MPD sequence number.
When a maintenance task is added by Everts and not part of the Boeing MD-80 MPD it will be identified by the three letter code TNK in the middle 3 digits of the task number.
2. AMM Reference.
Airplane Maintenance Manual procedure (Chapter, Section, Subject) which supports the MPD require-ment.
3. PGM.
Indicates program, (i.e. S = Structures Item, C = Corrosion item, and F = Fatigue item).
4. Zone.
The Zone identifies where the task is performed on the airplane.
5. Access.
The access panel or door number required to be opened when performing the task.
6. Interval.
Task intervals are expressed in terms of frequency and usage parameter such as calendar time and cycles.
a. Threshold: The initial interval that the task is to be performed.
b. Repeat: The repeat interval after the threshold interval has been reached.
i. FC = Airplane Flight Cycles.
ii. DY = Days.
iii. ENG CHG = Engine Change.
iv. LDG CHG = Landing Gear Change.
v. LIF LIM = Life Limited.
vi. NAT REQ = Regulatory Authority Requirement.
7. Interval Version.
• 1.1 - Threshold/Repeat 8000 cycles/ 8000 cycles.
• 1.2 - Threshold/Repeat 1500 days / 1500 days.
• 2.1 - Threshold/Repeat 28000 cycles / 4000 cycles.
• 2.2 - Threshold/Repeat 5250 days / 750 days.
The initial threshold of the task is 8000 cycles or 1500 days, whichever comes first. The task is initially repeated every 8000 cycles or 1500 days, whichever comes first, until the threshold of 28000 cycles or 5250 days, whichever comes first, is reached. The task is performed and then repeated at 4000 cycles or 750 days, whichever comes first.
8. Applicability.
Airplane (APL) Model:
• ALL = All Airplanes.
• NOTE = Airplane Applicability Note.
Engine (ENG):
• ALL = All Engines.
Rev 0 19 March 2014
3-7
MD-80 MAINTENANCE MANUAL
• Note = Engine Applicability Note.
9. Manhours.
Estimated labor hours required to perform the task. The estimates do not include labor hours for perform-ing the following functions:
• Docking the aircraft.
• Positioning/removing work stands.
• Access door/panel removal and installation.
• Cabin equipment, lining, floor panel and insulation removal and installation.
• Defueling, purging and refueling fuel tanks.
• Correcting discrepancies found while performing the task.
The estimates are based on the use of skilled personnel and assume that inspections in the same zone with a common frequency will be performed together.
10. Task Description.
The type of inspection that is accomplished and a description of the task to be performed. Applicability, Access and Interval notes are listed here to provide additional explanation for the other columns where “NOT” is used.
Rev 0 19 March 2014
3-8
MD-80 MAINTENANCE MANUAL
0 1 2 3 4 6A
TA 5
2: D
OO
RS
U7
52-0
01-0
252
-05-
03-2
11C
46N
OTE
96 M
O96
MO
ALL
ALL
0.67
INTE
RN
AL
- DE
TAIL
ED
: Mai
n E
ntra
nce
Doo
rD
o a
Det
aile
d In
spec
tion
of th
e M
ain
Ent
ranc
e D
oor,
STA
160
- 20
0, In
tern
al S
truct
ure
AC
CE
SS
NO
TE: P
eel b
ack
and/
or re
mov
e lin
ing
and/
or
insu
latio
n as
requ
ired.
U8
52-0
02-0
252
-05-
03-2
11C
58 59N
OTE
72 M
O72
MO
ALL
ALL
1.00
INTE
RN
AL
- DE
TAIL
ED
: Aft
Cab
in B
ulkh
ead
Doo
rD
o a
Det
aile
d In
spec
tion
of th
e A
ft C
abin
Pre
ssur
e B
ulkh
ead
Doo
r, S
TA 1
338
(MD
-87,
STA
112
9), I
nter
nal S
truct
ure
AC
CE
SS
NO
TE: P
eel b
ack
and/
or re
mov
e lin
ing
and/
or
insu
latio
n as
requ
ired.
U9
52-0
03-0
252
-05-
03-2
11C
58N
OTE
96 M
O96
MO
ALL
ALL
0.67
INTE
RN
AL
- DE
TAIL
ED
: Em
erge
ncy
Exi
t, O
verw
ing
Do
a D
etai
led
Insp
ectio
n of
the
Em
erge
ncy
Exi
t, O
verw
ing,
STA
86
4 - 9
27 (M
D-8
7, S
TA 7
50 -
813)
, Int
erna
l Stru
ctur
e
AC
CE
SS
NO
TE: P
eel b
ack
and/
or re
mov
e lin
ing
and/
or
insu
latio
n as
requ
ired.
U10
52-0
04-0
252
-05-
03-2
11C
51N
OTE
96 M
O96
MO
ALL
ALL
0.67
INTE
RN
AL
- DE
TAIL
ED
: For
war
d Lo
wer
Car
go D
oor
Do
a D
etai
led
Insp
ectio
n of
the
Doo
r, Fo
rwar
d Lo
wer
Car
go,
STA
370
- 42
7 (M
D-8
7, S
TA 3
13 -
370)
, Int
erna
l Stru
ctur
e
AC
CE
SS
NO
TE: P
eel b
ack
and/
or re
mov
e lin
ing
and/
or
insu
latio
n as
requ
ired.
U11
52-0
05-0
252
-05-
03-2
11C
51N
OTE
96 M
O96
MO
ALL
ALL
0.67
INTE
RN
AL
- DE
TAIL
ED
: Cen
ter L
ower
Car
go D
oor
Do
a D
etai
led
Insp
ectio
n of
the
Doo
r, C
ente
r Low
er C
argo
, STA
63
6 - 6
93 (M
D-8
7, S
TA 5
22 -
579)
, Int
erna
l Stru
ctur
e
AC
CE
SS
NO
TE: P
eel b
ack
and/
or re
mov
e lin
ing
and/
or
insu
latio
n as
requ
ired.
DC
-9-8
0SF
Mai
nten
ance
Pla
nnin
g D
ocum
ent
STR
UC
TUR
AL
MA
INTE
NA
NC
E PR
OG
RA
M
MPD
ITEM
NU
MB
ERAM
M
REF
EREN
CE
P G MZO
NE
ACC
ESS
INTE
RVA
L
THR
ES.
REP
EAT
APPL
ICAB
ILIT
Y
APL
ENG
MAN
-N
OITPIR
CSED
KSATS
RU
OH
Rev 0 19 March 2014
3-9
MD-80 MAINTENANCE MANUAL
0 1 2 3 4
DC
-9-8
0SF
Mai
nten
ance
Pla
nnin
g D
ocum
ent
STR
UC
TUR
AL
MA
INTE
NA
NC
E PR
OG
RA
M
MPD
ITEM
NU
MB
ERAM
M
REF
EREN
CE
P G MZO
NE
ACC
ESS
INTE
RVA
L
THR
ES.
REP
EAT
APPL
ICAB
ILIT
Y
APL
ENG
MAN
-N
OITPIR
CSED
KSATS
RU
OH
U12
52-0
06-0
252
-05-
03-2
11C
57N
OTE
96 M
O96
MO
ALL
ALL
0.67
INTE
RN
AL
- DE
TAIL
ED
: Aft
Low
er C
argo
Doo
rD
o a
Det
aile
d In
spec
tion
of th
e D
oor,
Aft
Low
er C
argo
, STA
11
56 -
1211
(MD
-87,
STA
103
0 - 1
070)
, Int
erna
l Stru
ctur
e
AC
CE
SS
NO
TE: P
eel b
ack
and/
or re
mov
e lin
ing
and/
or
insu
latio
n as
requ
ired.
U13
52-0
07-0
252
-05-
03-2
11C
45N
OTE
96 M
O96
MO
ALL
ALL
0.67
INTE
RN
AL
- DE
TAIL
ED
: Ele
ctric
al /
Ele
ctro
nics
Com
partm
ent
Doo
rD
o a
Det
aile
d In
spec
tion
of th
e D
oor,
Ele
ctric
al /
Ele
ctro
nics
C
ompa
rtmen
t, S
TA 1
48, I
nter
nal S
truct
ure
AC
CE
SS
NO
TE: P
eel b
ack
and/
or re
mov
e lin
ing
and/
or
insu
latio
n as
requ
ired.
U14
52-0
08-0
252
-05-
03-2
11C
46N
OTE
96 M
O96
MO
ALL
ALL
1.00
INTE
RN
AL
- DE
TAIL
ED
: For
war
d G
alle
y S
ervi
ce D
oor
Do
a D
etai
led
Insp
ectio
n of
the
Doo
r, Fo
rwar
d G
alle
y S
ervi
ce,
STA
168
- 20
0, In
tern
al S
truct
ure
AC
CE
SS
NO
TE: P
eel b
ack
and/
or re
mov
e lin
ing
and/
or
insu
latio
n as
requ
ired.
U15
52-0
09-0
252
-05-
03-2
11C
58N
OTE
72 M
O72
MO
ALL
ALL
1.00
INTE
RN
AL
- DE
TAIL
ED
: Aft
Gal
ley
Ser
vice
Doo
rD
o a
Det
aile
d In
spec
tion
of th
e D
oor,
Aft
Gal
ley
Ser
vice
, STA
11
40 -
1170
(MD
-87,
STA
949
- 97
9), I
nter
nal S
truct
ure
AC
CE
SS
NO
TE: P
eel b
ack
and/
or re
mov
e lin
ing
and/
or
insu
latio
n as
requ
ired.
U16
52-0
10-0
252
-05-
03-2
11C
42N
OTE
96 M
O96
MO
ALL
ALL
0.25
INTE
RN
AL
- DE
TAIL
ED
: For
war
d A
cces
sory
Com
partm
ent
Doo
rD
o a
Det
aile
d In
spec
tion
of th
e Fo
rwar
d A
cces
sory
C
ompa
rtmen
t Doo
r, S
TA 4
1 - 6
9, In
tern
al S
truct
ure
AC
CE
SS
NO
TE: P
eel b
ack
and/
or re
mov
e lin
ing
and/
or
insu
latio
n as
requ
ired.
U17
52-1
11-0
252
-05-
03-2
11C
55 56N
OTE
72 M
O72
MO
ALL
ALL
0.50
INTE
RN
AL
- DE
TAIL
ED
: Mai
n La
ndin
g G
ear D
oors
Do
a D
etai
led
Insp
ectio
n of
the
Mai
n La
ndin
g G
ear D
oors
STA
94
6 - 1
003
(MD
-87,
STA
832
- 88
9, In
tern
al S
truct
ure
AC
CE
SS
NO
TE: P
eel b
ack
and/
or re
mov
e lin
ing
and/
or
insu
latio
n as
requ
ired.
Rev 0 19 March 2014
3-10
MD-80 MAINTENANCE MANUAL
0 1 2 3 4
DC
-9-8
0SF
Mai
nten
ance
Pla
nnin
g D
ocum
ent
STR
UC
TUR
AL
MA
INTE
NA
NC
E PR
OG
RA
M
MPD
ITEM
NU
MB
ERAM
M
REF
EREN
CE
P G MZO
NE
ACC
ESS
INTE
RVA
L
THR
ES.
REP
EAT
APPL
ICAB
ILIT
Y
APL
ENG
MAN
-N
OITPIR
CSED
KSATS
RU
OH
U18
52-1
12-0
252
-05-
03-2
11C
17 18N
OTE
72 M
O72
MO
ALL
ALL
0.33
INTE
RN
AL
- DE
TAIL
ED
: Mai
n G
ear S
trut,
Doo
rsD
o a
Det
aile
d In
spec
tion
of th
e Le
ft an
d R
ight
Mai
n G
ear S
trut,
Doo
rs S
truct
ure
AC
CE
SS
NO
TE: P
eel b
ack
and/
or re
mov
e lin
ing
and/
or
insu
latio
n as
requ
ired.
19A
TA 5
3: F
USE
LAG
E
U20
53-0
03-0
053
-05-
03-2
11S
55 56N
OTE
NO
TEA
LLA
LL4.
00E
XTE
RN
AL
- DE
TAIL
ED
: Sla
nt P
ress
ure
Pan
elD
etai
led
Insp
ectio
n of
the
Sla
nt P
ress
ure
Pan
el
INTE
RV
AL
NO
TE: R
efer
to A
D 2
003-
09-0
7 an
d S
B D
C9-
53A
295
for r
epet
itive
inte
rval
s.
U21
53-0
13-0
253
-05-
03-2
11C
4243
02A
NO
TE96
MO
96 M
OA
LLA
LL0.
33IN
TER
NA
L - D
ETA
ILE
D: F
orw
ard
Acc
esso
ry C
ompa
rtmen
t D
oor J
amb
Do
a D
etai
led
insp
ectio
n of
the
Forw
ard
Acc
esso
ry
Com
partm
ent D
oor J
amb
AC
CE
SS
NO
TE: P
eel b
ack
and/
or re
mov
e lin
ing
and/
or
insu
latio
n as
requ
ired.
U22
53-0
14-0
253
-05-
03-2
11C
4545
01A
NO
TE48
MO
48 M
OA
LLA
LL0.
50IN
TER
NA
L - D
ETA
ILE
D: E
/E C
ompa
rtmen
t Doo
r Jam
bD
o a
Det
aile
d in
spec
tion
of th
e of
the
E/E
Com
partm
ent D
oor
Jam
b In
tern
al S
truct
ure
AC
CE
SS
NO
TE: P
eel b
ack
and/
or re
mov
e lin
ing
and/
or
insu
latio
n as
requ
ired.
U23
53-0
15-0
253
-05-
03-2
11C
46N
OTE
96 M
O96
MO
ALL
ALL
0.67
INTE
RN
AL
- DE
TAIL
ED
: Mai
n E
ntra
nce
Doo
r Jam
bD
o a
Det
aile
d in
spec
tion
of th
e M
ain
Ent
ranc
e D
oor J
amb,
In
tern
al S
truct
ure
AC
CE
SS
NO
TE: P
eel b
ack
and/
or re
mov
e lin
ing
and/
or
insu
latio
n as
requ
ired.
U24
53-0
16-0
253
-05-
03-2
11C
46N
OTE
96 M
O96
MO
ALL
ALL
0.67
INTE
RN
AL
- DE
TAIL
ED
: For
war
d G
alle
y S
ervi
ce D
oor J
amb
Do
a D
etai
led
Insp
ectio
n of
the
Forw
ard
Gal
ley
Ser
vice
Doo
r Ja
mb,
Inte
rnal
Stru
ctur
e
AC
CE
SS
NO
TE: P
eel b
ack
and/
or re
mov
e lin
ing
and/
or
insu
latio
n as
requ
ired.
Rev 0 19 March 2014
3-11
MD-80 MAINTENANCE MANUAL
0 1 2 3 4
DC
-9-8
0SF
Mai
nten
ance
Pla
nnin
g D
ocum
ent
STR
UC
TUR
AL
MA
INTE
NA
NC
E PR
OG
RA
M
MPD
ITEM
NU
MB
ERAM
M
REF
EREN
CE
P G MZO
NE
ACC
ESS
INTE
RVA
L
THR
ES.
REP
EAT
APPL
ICAB
ILIT
Y
APL
ENG
MAN
-N
OITPIR
CSED
KSATS
RU
OH
U25
53-0
16-0
405
-21-
01-2
80F
4615
000
FC15
000
FCAL
LAL
L0.
67IN
TER
NA
L - S
PEC
IAL
DET
AILE
D: F
orw
ard
Gal
ley
Serv
ice
Doo
r Jam
bD
o a
Spe
cial
Det
aile
d In
spec
tion
of th
e Fo
rwar
d G
alle
y S
ervi
ce
Doo
r Jam
b, X
-ray
Upp
er F
orw
ard
Cor
ner
SP
EC
IAL
NO
TE: R
efer
to N
DT
Sta
ndar
d P
ract
ice
Man
ual,
Par
t 02
, pro
cedu
re 1
, 02-
10-0
1.00
1, p
age
1.
U26
53-0
17-0
253
-05-
03-2
11C
51N
OTE
48 M
O48
MO
ALL
ALL
0.67
INTE
RN
AL
- DE
TAIL
ED
: Jam
b, F
orw
ard
Low
er C
argo
C
ompa
rtmen
t Doo
rD
o a
Det
aile
d In
spec
tion
of th
e Ja
mb,
Fw
d Lw
r Car
go C
ompt
D
oor,
STA
370
- 42
7 (M
D-8
7, S
TA 3
13 -
370)
Inte
rnal
Stru
ctur
e
ACC
ESS
NO
TE: W
ith s
cuff
plat
e re
mov
ed. P
eel b
ack
and/
or
rem
ove
linin
g an
d/or
insu
latio
n as
requ
ired.
U27
53-0
18-0
253
-05-
03-2
11C
51N
OTE
48 M
O48
MO
ALL
ALL
0.67
INTE
RN
AL
- DE
TAIL
ED
: Jam
b, C
ente
r Low
er C
argo
C
ompa
rtmen
t Doo
rD
o a
Det
aile
d In
spec
tion
of th
e Ja
mb,
Cnt
r Lw
r Car
go C
ompt
D
oor,
STA
636
- 69
3 (M
D-8
7, S
TA 5
22 -
579)
Inte
rnal
Stru
ctur
e
ACC
ESS
NO
TE: W
ith s
cuff
plat
e re
mov
ed. P
eel b
ack
and/
or
rem
ove
linin
g an
d/or
insu
latio
n as
requ
ired.
U28
53-0
19-0
253
-05-
03-2
11C
57N
OTE
48 M
O48
MO
ALL
ALL
0.67
INTE
RN
AL
- DE
TAIL
ED
: Jam
b, A
ft Lo
wer
Car
go C
ompa
rtmen
t D
oor
Do
a D
etai
led
Insp
ectio
n of
the
Jam
b, A
ft Lw
r Car
go C
ompt
D
oor,
STA
115
4 - 1
211
(MD
-87,
STA
964
- 10
02) I
nter
nal
Stru
ctur
e
AC
CE
SS
NO
TE: P
eel b
ack
and/
or re
mov
e lin
ing
and/
or
insu
latio
n as
requ
ired.
U29
53-0
20-0
253
-05-
03-2
11C
58N
OTE
72 M
O72
MO
ALL
ALL
1.00
INTE
RN
AL
- DE
TAIL
ED
: Jam
b, A
ft G
alle
y S
ervi
ce D
oor
Do
a D
etai
led
Insp
ectio
n of
the
Jam
b, A
ft G
alle
y S
ervi
ce D
oor,
STA
114
0 - 1
170
(MD
-87,
STA
950
- 98
0) In
tern
al S
truct
ure
AC
CE
SS
NO
TE: P
eel b
ack
and/
or re
mov
e lin
ing
and/
or
insu
latio
n as
requ
ired.
Rev 0 19 March 2014
3-12
MD-80 MAINTENANCE MANUAL
0 1 2 3 4
DC
-9-8
0SF
Mai
nten
ance
Pla
nnin
g D
ocum
ent
STR
UC
TUR
AL
MA
INTE
NA
NC
E PR
OG
RA
M
MPD
ITEM
NU
MB
ERAM
M
REF
EREN
CE
P G MZO
NE
ACC
ESS
INTE
RVA
L
THR
ES.
REP
EAT
APPL
ICAB
ILIT
Y
APL
ENG
MAN
-N
OITPIR
CSED
KSATS
RU
OH
U30
53-0
21-0
353
-05-
03-2
11C
58 59N
OTE
72 M
O72
MO
ALL
ALL
0.67
INTE
RN
AL
- DE
TAIL
ED
: Aft
Cab
in B
ulkh
ead
Doo
rD
o a
Det
aile
d In
spec
tion
of th
e A
ft C
abin
Bul
khea
d D
oor J
amb,
S
TA 1
338
(MD
-87,
STA
112
9)
AC
CE
SS
NO
TE: P
eel b
ack
and/
or re
mov
e lin
ing
and/
or
insu
latio
n as
requ
ired.
U31
53-0
22-0
253
-05-
03-2
11C
55 56N
OTE
72 M
O72
MO
ALL
ALL
1.33
INTE
RN
AL
- DE
TAIL
ED
: Tra
pezo
idal
Pan
elD
o a
Det
aile
d In
spec
tion
of th
e P
anel
, Tra
pezo
idal
, STA
937
- 96
5 (M
D-8
7, S
TA 8
23 -
851)
, Stru
ctur
e
AC
CE
SS
NO
TE: P
eel b
ack
and/
or re
mov
e lin
ing
and/
or
insu
latio
n as
requ
ired.
U32
53-0
23-0
253
-05-
03-2
11C
55 56N
OTE
72 M
O72
MO
ALL
ALL
1.00
INTE
RN
AL
- DE
TAIL
ED
: Lon
gero
n N
o. 2
0, A
ft en
d of
Tr
apez
oida
l Pan
elD
o a
Det
aile
d In
spec
tion
of th
e Lo
nger
on N
o. 2
0, A
ft en
d of
Tr
ap P
anel
, STA
965
- 10
03 (M
D-8
7, S
TA 8
51 -
889)
, Stru
ctur
e
AC
CE
SS
NO
TE: P
eel b
ack
and/
or re
mov
e lin
ing
and/
or
insu
latio
n as
requ
ired.
U33
53-0
24-0
253
-05-
03-2
11C
21 2221
16C
2216
CN
OTE
72 M
O72
MO
ALL
ALL
1.33
INTE
RN
AL
- DE
TAIL
ED
: Lon
gero
n N
o. 2
4, W
ing
To F
usel
age
Fitti
ngD
o a
Det
aile
d In
spec
tion
of th
e Lo
nger
on N
o. 2
4, W
ing
To
Fuse
lage
Fitt
ing,
incl
udin
g ar
ea u
nder
Fille
t Fai
rings
, STA
826
(M
D-8
7, S
TA 7
12) I
nter
nal S
truct
ure
AC
CE
SS
NO
TE: P
eel b
ack
and/
or re
mov
e lin
ing
and/
or
insu
latio
n as
requ
ired.
U34
53-0
25-0
253
-05-
03-2
11C
53N
OTE
96 M
O96
MO
ALL
ALL
1.33
INTE
RN
AL
- DE
TAIL
ED
: Fus
elag
e Fr
ames
, Ove
rwin
gD
o a
Det
aile
d In
spec
tion
of th
e Fu
sela
ge F
ram
es, O
verw
ing,
S
TA's
864
, 886
&90
5 (M
D-8
7, S
TA's
750
, 772
&79
1) In
tern
al
Stru
ctur
e
AC
CE
SS
NO
TE: P
eel b
ack
and/
or re
mov
e lin
ing
and/
or
insu
latio
n as
requ
ired.
Cab
in, c
ente
r win
g ar
ea: R
emov
e se
ats,
ca
rpet
and
floo
r pan
els.
Rev 0 19 March 2014
3-13
MD-80 MAINTENANCE MANUAL
0 1 2 3 4
DC
-9-8
0SF
Mai
nten
ance
Pla
nnin
g D
ocum
ent
STR
UC
TUR
AL
MA
INTE
NA
NC
E PR
OG
RA
M
MPD
ITEM
NU
MB
ERAM
M
REF
EREN
CE
P G MZO
NE
ACC
ESS
INTE
RVA
L
THR
ES.
REP
EAT
APPL
ICAB
ILIT
Y
APL
ENG
MAN
-N
OITPIR
CSED
KSATS
RU
OH
U35
53-0
26-0
253
-05-
03-2
11C
55 56N
OTE
72 M
O72
MO
ALL
ALL
1.50
INTE
RN
AL
- DE
TAIL
ED
: Fus
elag
e Fr
ame,
Ove
r Tra
pezo
idal
P
anel
Do
a D
etai
led
Insp
ectio
n of
the
Fuse
lage
Fra
me,
Ove
r Tr
apez
oida
l Pan
el, S
TA 9
65 (M
D-8
7, S
TA 8
51),
Stru
ctur
e
AC
CE
SS
NO
TE: P
eel b
ack
and/
or re
mov
e lin
ing
and/
or
insu
latio
n as
requ
ired.
U36
53-0
27-0
253
-05-
03-2
11C
58N
OTE
72 M
O72
MO
ALL
ALL
1.50
INTE
RN
AL
- DE
TAIL
ED
: Aft
Cab
in F
usel
age
Cei
ling
Abo
ve
Lavs
&G
alle
ysD
o a
Det
aile
d In
spec
tion
of th
e Fr
ames
, Aft
Cab
in F
usel
age
Cei
ling
Abo
ve L
avs&
Gal
leys
, (La
vs&
Gal
leys
Rem
oved
) STA
12
71 -
1338
(MD
-87,
STA
106
2 - 1
129)
Inte
rnal
Stru
ctur
e
AC
CE
SS
NO
TE: L
avs&
Gal
leys
Rem
oved
. Pee
l bac
k an
d/or
re
mov
e lin
ing
and/
or in
sula
tion
as re
quire
d.
U37
53-0
28-0
253
-05-
03-2
11C
5421
10C
2116
C22
10C
2216
CN
OTE
96 M
O96
MO
ALL
ALL
0.75
INTE
RN
AL
- DE
TAIL
ED
: Kee
l, U
nder
win
g B
arre
lD
o a
Det
aile
d In
spec
tion
of th
e K
eel,
Und
erw
ing
Bar
rel,
STA
81
7 - 9
46 (M
D-8
7, S
TA 7
03 -
832)
, Int
erna
l Stru
ctur
e
AC
CE
SS
NO
TE: P
eel b
ack
and/
or re
mov
e lin
ing
and/
or
insu
latio
n as
requ
ired.
U38
53-0
29-0
253
-05-
03-2
11C
55 56N
OTE
72 M
O72
MO
ALL
ALL
1.33
INTE
RN
AL
- DE
TAIL
ED
: Kee
l, M
LG W
heel
Wel
lD
o a
Det
aile
d In
spec
tion
of th
e K
eel,
MLG
Whe
el W
ell,
STA
94
6 - 1
003
(MD
-87,
STA
832
- 88
9), S
truct
ure
AC
CE
SS
NO
TE: P
eel b
ack
and/
or re
mov
e lin
ing
and/
or
insu
latio
n as
requ
ired.
U39
53-0
30-0
253
-05-
03-2
11C
57N
OTE
48 M
O48
MO
ALL
ALL
0.67
INTE
RN
AL
- DE
TAIL
ED
: Pre
ssur
e B
ulkh
ead,
MLG
Whe
el W
ell
Do
a D
etai
led
Insp
ectio
n of
the
Pre
ssur
e B
ulkh
ead,
MLG
Whe
el
Wel
l, S
TA 1
003
and
1007
(MD
-87,
STA
889
and
893
) Aft
Face
AC
CE
SS
NO
TE: P
eel b
ack
and/
or re
mov
e lin
ing
and/
or
insu
latio
n as
requ
ired.
Rev 0 19 March 2014
3-14
MD-80 MAINTENANCE MANUAL
0 1 2 3 4
DC
-9-8
0SF
Mai
nten
ance
Pla
nnin
g D
ocum
ent
STR
UC
TUR
AL
MA
INTE
NA
NC
E PR
OG
RA
M
MPD
ITEM
NU
MB
ERAM
M
REF
EREN
CE
P G MZO
NE
ACC
ESS
INTE
RVA
L
THR
ES.
REP
EAT
APPL
ICAB
ILIT
Y
APL
ENG
MAN
-N
OITPIR
CSED
KSATS
RU
OH
U40
53-0
31-0
253
-05-
03-2
11C
57 58 59
5703
C57
18C
NO
TE
72 M
O72
MO
ALL
ALL
1.87
INTE
RN
AL
- DE
TAIL
ED
: Pre
ssur
e B
ulkh
ead,
Ven
tral S
tair
Do
a D
etai
led
Insp
ectio
n of
the
Pre
ssur
e B
ulkh
ead,
Ven
tral
Sta
ir, S
TA 1
338
(MD
-87,
STA
112
9), S
truct
ure
AC
CE
SS
NO
TE: P
eel b
ack
and/
or re
mov
e lin
ing
and/
or
insu
latio
n as
requ
ired.
U41
53-0
32-0
253
-05-
03-2
11C
58N
OTE
72 M
O72
MO
ALL
ALL
0.83
INTE
RN
AL
- DE
TAIL
ED
: Aft
Lava
tory
Eng
ine
Pyl
on S
uppo
rtD
o a
Det
aile
d In
spec
tion
of th
e B
ulkh
ead,
Aft
Lava
tory
Eng
ine
Pyl
on S
uppo
rt, S
TA 1
307
(MD
-87,
STA
109
8) In
tern
al S
truct
ure
AC
CE
SS
NO
TE: P
eel b
ack
and/
or re
mov
e lin
ing
and/
or
insu
latio
n as
requ
ired.
U42
53-0
33-0
253
-05-
03-2
11C
5996
MO
96 M
OA
LLA
LL0.
67IN
TER
NA
L - D
ETA
ILE
D: A
ft A
cces
sory
Com
partm
ent E
ngin
e P
ylon
Sup
port
Do
a D
etai
led
Insp
ectio
n of
the
Bul
khea
d, A
ft A
ccy
Com
pt E
ng
Pyl
on S
pt, S
TA 1
380
(MD
-87
STA
117
1), I
nter
nal S
truct
ure
U43
53-0
34-0
253
-05-
03-2
11C
50N
OTE
96 M
O96
MO
ALL
ALL
0.40
EXT
ER
NA
L - D
ETA
ILE
D: A
ttach
Ang
le, T
op F
usel
age
To
Ver
tical
Sta
biliz
er J
oint
Do
a D
etai
led
Insp
ectio
n of
the
Atta
ch A
ngle
, Top
Fus
To
Ver
t S
tab
Join
t, S
TA 1
401-
1429
(MD
-87,
STA
119
2-12
20),
Ext
erna
l S
truct
ure
AC
CE
SS
NO
TE: P
eel b
ack
and/
or re
mov
e lin
ing
and/
or
insu
latio
n as
requ
ired.
U44
53-0
35-0
253
-05-
03-2
11C
60N
OTE
96 M
O96
MO
ALL
ALL
0.40
EXT
ER
NA
L - D
ETA
ILE
D: A
ttach
Ang
le, T
op F
usel
age
To
Ver
tical
Sta
biliz
er J
oint
Do
a D
etai
led
Insp
ectio
n of
the
Atta
ch A
ngle
, Top
Fus
To
Ver
t S
tab
Join
t, S
TA 1
429-
1474
(MD
-87,
STA
122
0-12
65),
Ext
erna
l S
truct
ure
AC
CE
SS
NO
TE: P
eel b
ack
and/
or re
mov
e lin
ing
and/
or
insu
latio
n as
requ
ired.
U45
53-0
36-0
253
-05-
03-2
11C
60 61N
OTE
96 M
O96
MO
ALL
ALL
0.33
INTE
RN
AL
- DE
TAIL
ED
: Can
ted
Fram
eD
o a
Det
aile
d In
spec
tion
of th
e C
ante
d Fr
ame,
STA
148
5 (M
D-
87, S
TA 1
276)
, Int
erna
l Stru
ctur
e
AC
CE
SS
NO
TE: P
eel b
ack
and/
or re
mov
e lin
ing
and/
or
insu
latio
n as
requ
ired.
Rev 0 19 March 2014
3-15
MD-80 MAINTENANCE MANUAL
0 1 2 3 4
DC
-9-8
0SF
Mai
nten
ance
Pla
nnin
g D
ocum
ent
STR
UC
TUR
AL
MA
INTE
NA
NC
E PR
OG
RA
M
MPD
ITEM
NU
MB
ERAM
M
REF
EREN
CE
P G MZO
NE
ACC
ESS
INTE
RVA
L
THR
ES.
REP
EAT
APPL
ICAB
ILIT
Y
APL
ENG
MAN
-N
OITPIR
CSED
KSATS
RU
OH
U46
53-0
37-0
153
-05-
03-2
11C
45 46 51 53 57 58
NO
TE96
MO
96 M
OA
LLA
LL5.
53IN
TER
NA
L - D
ETA
ILE
D: F
loor
Bea
ms&
Sea
t Tra
cks
Do
a D
etai
led
Insp
ectio
n of
the
Floo
r Bea
ms&
Sea
t Tra
cks
(Lav
s, G
alle
ys&
Floo
r Pan
els
Rem
oved
) STA
148
.5-1
306
(MD
-87
, STA
148
.5-1
096)
, Int
erna
l Stru
ctur
e
AC
CE
SS
NO
TE: L
avs,
Gal
leys
and
Flo
or P
anel
s R
emov
ed.
U47
53-0
38-0
253
-05-
03-2
11C
44 46N
OTE
96 M
O96
MO
ALL
ALL
0.37
INTE
RN
AL
- DE
TAIL
ED
: Ski
n P
anel
s, C
abin
Flo
orD
o a
Det
aile
d In
spec
tion
of th
e S
kin
Pan
els,
STA
69
- 218
, In
tern
al S
truct
ure
(Lon
gero
n 18
L-18
R, A
bove
Cab
in F
loor
AC
CE
SS
NO
TE: P
eel b
ack
and/
or re
mov
e lin
ing
and/
or
insu
latio
n as
requ
ired.
U48
53-0
38-0
353
-05-
03-2
11C
45N
OTE
96 M
O96
MO
ALL
ALL
0.25
INTE
RN
AL
- DE
TAIL
ED
: Ski
n P
anel
s, B
elow
Cab
in F
loor
Do
a D
etai
led
Insp
ectio
n of
the
Ski
n P
anel
s, S
TA 6
9 - 2
18,
Inte
rnal
Stru
ctur
e (L
onge
ron
18L-
27L,
18R
-27R
, Bel
ow C
abin
Fl
oor)
AC
CE
SS
NO
TE: P
eel b
ack
and/
or re
mov
e lin
ing
and/
or
insu
latio
n as
requ
ired.
U49
53-0
38-0
453
-05-
03-2
11C
45N
OTE
48 M
O48
MO
ALL
ALL
0.25
INTE
RN
AL
- DE
TAIL
ED
: Ski
n P
anel
s, B
ilge
Are
aD
o a
Det
aile
d In
spec
tion
of th
e S
kin
Pan
els,
STA
110
- 21
8,
Inte
rnal
Stru
ctur
e (L
onge
ron
27L-
27R
, Bilg
e A
rea)
AC
CE
SS
NO
TE: P
eel b
ack
and/
or re
mov
e lin
ing
and/
or
insu
latio
n as
requ
ired.
U50
53-0
38-0
553
-05-
03-2
11C
42N
OTE
96 M
O96
MO
ALL
ALL
0.08
INTE
RN
AL
- DE
TAIL
ED
: Ski
n P
anel
s, A
bove
Pre
ssur
e P
anel
Do
a D
etai
led
Insp
ectio
n of
the
Ski
n P
anel
s, In
tern
al S
truct
ure
(Abo
ve P
ress
ure
Pan
el, S
TA 3
7-69
).
AC
CE
SS
NO
TE: P
eel b
ack
and/
or re
mov
e lin
ing
and/
or
insu
latio
n as
requ
ired.
U51
53-0
38-0
653
-05-
03-2
11C
43N
OTE
72 M
O72
MO
ALL
ALL
0.08
INTE
RN
AL
- DE
TAIL
ED
: Ski
n P
anel
s, S
TA 3
7 - 1
10, I
nter
nal
Stru
ctur
e (N
ose
Whe
el W
ell)
Do
a D
etai
led
Insp
ectio
n of
the
Ski
n P
anel
s, S
TA 3
7 - 1
10,
Inte
rnal
Stru
ctur
e (N
ose
Whe
el W
ell)
AC
CE
SS
NO
TE: P
eel b
ack
and/
or re
mov
e lin
ing
and/
or
insu
latio
n as
requ
ired.
Rev 0 19 March 2014
3-16
MD-80 MAINTENANCE MANUAL
0 1 2 3 4
DC
-9-8
0SF
Mai
nten
ance
Pla
nnin
g D
ocum
ent
STR
UC
TUR
AL
MA
INTE
NA
NC
E PR
OG
RA
M
MPD
ITEM
NU
MB
ERAM
M
REF
EREN
CE
P G MZO
NE
ACC
ESS
INTE
RVA
L
THR
ES.
REP
EAT
APPL
ICAB
ILIT
Y
APL
ENG
MAN
-N
OITPIR
CSED
KSATS
RU
OH
U52
53-0
39-0
253
-05-
03-2
11C
43N
OTE
72 M
O72
MO
ALL
ALL
0.33
INTE
RN
AL
- DE
TAIL
ED
: NLG
Ret
ract
Cyl
inde
r Atta
ch F
ittin
gD
o a
Det
aile
d In
spec
tion
of th
e N
LG R
etra
ct C
ylin
der A
ttach
Fi
tting
, STA
110
, Stru
ctur
e
AC
CE
SS
NO
TE: P
eel b
ack
and/
or re
mov
e lin
ing
and/
or
insu
latio
n as
requ
ired.
U53
53-0
40-0
253
-05-
03-2
11C
55 56N
OTE
72 M
O72
MO
ALL
ALL
1.00
INTE
RN
AL
- DE
TAIL
ED
: Fitt
ing,
Kee
l To
Rea
r Win
g S
par
Do
a D
etai
led
Insp
ectio
n of
the
Fitti
ng, K
eel T
o R
ear W
ing
Spa
r, S
TA 9
46 (M
D-8
7, S
TA 8
32),
Stru
ctur
e
AC
CE
SS
NO
TE: P
eel b
ack
and/
or re
mov
e lin
ing
and/
or
insu
latio
n as
requ
ired.
U54
53-0
41-0
253
-05-
03-2
11C
55 5672
MO
72 M
OA
LLA
LL0.
67IN
TER
NA
L - D
ETA
ILE
D: F
ittin
g, R
etra
ct C
ylin
der M
LG D
oor
Do
a D
etai
led
Insp
ectio
n of
the
Fitti
ng, R
etra
ct C
ylin
der M
LG
Doo
r, S
TA 9
46 (M
D-8
7, S
TA 8
32),
Stru
ctur
e
U55
53-0
42-0
253
-05-
03-2
11C
6159
10A
6301
A96
MO
96 M
OA
LLA
LL0.
50IN
TER
NA
L - D
ETA
ILE
D: D
orsa
l Fitt
ing,
Ver
tical
Sta
biliz
erD
o a
Det
aile
d In
spec
tion
of th
e D
orsa
l Fitt
ing,
Ver
tical
S
tabi
lizer
, STA
143
7 (M
D-8
7, S
TA 1
228)
, Int
erna
l Stru
ctur
e
U56
53-1
03-0
253
-05-
03-2
11C
5196
MO
96 M
OA
LLA
LL0.
10IN
TER
NA
L - D
ETA
ILE
D: F
wd
Aux
Fue
l Tan
k A
ft B
ulkh
ead
Do
a D
etai
led
Insp
ectio
n of
the
Fwd
Aux
Fue
l Tan
k A
ft B
ulkh
ead,
STA
596
(MD
-87,
STA
482
), In
spec
t Bul
khea
d ar
ound
acc
ess
hole
cut
out
U57
53-1
39-0
205
-21-
01-2
11C
58N
OTE
96 M
O96
MO
ALL
ALL
8.00
INTE
RN
AL
- DE
TAIL
ED
: Ski
n P
anel
s, S
TA 2
18-1
338
(MD
-87,
S
TA 2
18-1
129)
Do
a D
etai
led
Insp
ectio
n of
the
Ski
n P
anel
s, S
TA 2
18-1
338
(MD
-87,
STA
218
-112
9), I
nter
nal S
truct
ure
excl
udin
g ar
eas
in
task
53-
139-
03-0
1
AC
CE
SS
NO
TE: P
eel b
ack
and/
or re
mov
e lin
ing
and/
or
insu
latio
n as
requ
ired.
Rev 0 19 March 2014
3-17
MD-80 MAINTENANCE MANUAL
0 1 2 3 4
DC
-9-8
0SF
Mai
nten
ance
Pla
nnin
g D
ocum
ent
STR
UC
TUR
AL
MA
INTE
NA
NC
E PR
OG
RA
M
MPD
ITEM
NU
MB
ERAM
M
REF
EREN
CE
P G MZO
NE
ACC
ESS
INTE
RVA
L
THR
ES.
REP
EAT
APPL
ICAB
ILIT
Y
APL
ENG
MAN
-N
OITPIR
CSED
KSATS
RU
OH
U58
53-1
39-0
305
-21-
01-2
11C
51 57 58
NO
TE96
MO
96 M
OA
LLA
LL3.
50IN
TER
NA
L - D
ETA
ILE
D: S
kin
Pan
els,
Und
er F
illet F
airin
g,
Ove
r Win
g E
mer
g E
xit A
rea,
Abo
ve C
abin
Flo
or S
plic
es,
Ant
enna
Cut
outs
Do
a D
etai
led
Insp
ectio
n of
the
Ski
n P
anel
s, S
TA 2
18-1
338
(MD
-87,
STA
218
-112
9), I
nter
nal S
truct
ure
(Are
a un
der F
illet
Fairi
ng, O
ver W
ing
Em
erge
ncy
Exi
t Are
a, A
bove
Cab
in F
loor
S
plic
es, U
pper
and
Low
er A
nten
na C
utou
ts a
s vi
ewed
from
The
ou
tsid
e&Lo
wer
from
Bilg
e A
rea
also
) (A
nten
na's
Rem
oved
)
AC
CE
SS
NO
TE: A
nten
na's
Rem
oved
. Pee
l bac
k an
d/or
re
mov
e lin
ing
and/
or in
sula
tion
as re
quire
d. R
emov
e lin
ing
in
carg
o co
mpa
rtmen
t as
requ
ired
to in
spec
t are
a un
der f
illet
fairi
ng.
U59
53-1
39-0
453
-05-
03-2
11C
51 57N
OTE
96 M
O96
MO
ALL
ALL
2.67
INTE
RN
AL
- DE
TAIL
ED
: Ski
n P
anel
s, b
elow
Cab
in F
loor
, 18L
-24
L, 1
8R-2
4RD
o a
Det
aile
d In
spec
tion
of th
e S
kin
Pan
els,
STA
218
-133
8 (M
D-8
7, S
TA 2
18-1
129)
, Int
erna
l Stru
ctur
e (b
elow
Cab
in F
loor
, 18
L-24
L, 1
8R-2
4R)
AC
CE
SS
NO
TE: P
eel b
ack
and/
or re
mov
e lin
ing
and/
or
insu
latio
n as
requ
ired.
U60
53-1
39-0
553
-05-
03-2
11C
51 57N
OTE
48 M
O48
MO
ALL
ALL
2.67
INTE
RN
AL
- DE
TAIL
ED
: Ski
n P
anel
s, b
elow
Cab
in F
loor
, 24L
-24
RD
o a
Det
aile
d In
spec
tion
of th
e S
kin
Pan
els,
STA
218
-133
8 (M
D-8
7, S
TA 2
18-1
129)
, Int
erna
l Stru
ctur
e (b
elow
Cab
in F
loor
, 24
L-24
R)
AC
CE
SS
NO
TE: P
eel b
ack
and/
or re
mov
e lin
ing
and/
or
insu
latio
n as
requ
ired.
U61
53-1
40-0
253
-05-
03-2
11C
59 61N
OTE
96 M
O96
MO
ALL
ALL
0.50
INTE
RN
AL
- DE
TAIL
ED
: Ski
n P
anel
s, U
pper
Fus
elag
eD
o a
Det
aile
d In
spec
tion
of th
e S
kin
Pan
els,
STA
133
8-16
33
(MD
-87,
STA
112
9-14
36),
Inte
rnal
Stru
ctur
e (U
pper
Fus
elag
e,
18L-
18R
)
AC
CE
SS
NO
TE: P
eel b
ack
and/
or re
mov
e lin
ing
and/
or
insu
latio
n as
requ
ired.
Rev 0 19 March 2014
3-18
MD-80 MAINTENANCE MANUAL
0 1 2 3 4
DC
-9-8
0SF
Mai
nten
ance
Pla
nnin
g D
ocum
ent
STR
UC
TUR
AL
MA
INTE
NA
NC
E PR
OG
RA
M
MPD
ITEM
NU
MB
ERAM
M
REF
EREN
CE
P G MZO
NE
ACC
ESS
INTE
RVA
L
THR
ES.
REP
EAT
APPL
ICAB
ILIT
Y
APL
ENG
MAN
-N
OITPIR
CSED
KSATS
RU
OH
U62
53-1
40-0
353
-05-
03-2
11C
59 61N
OTE
96 M
O96
MO
ALL
ALL
0.50
INTE
RN
AL
- DE
TAIL
ED
: Ski
n P
anel
s, L
ower
Fus
elag
eD
o a
Det
aile
d In
spec
tion
of th
e S
kin
Pan
els,
STA
133
8-16
33
(MD
-87,
STA
112
9-14
36),
Inte
rnal
Stru
ctur
e (L
ower
Fus
elag
e,
18L-
18R
)
AC
CE
SS
NO
TE: P
eel b
ack
and/
or re
mov
e lin
ing
and/
or
insu
latio
n as
requ
ired.
63A
TA 5
4: N
AC
ELLE
S/PY
LON
S
U64
54-0
44-0
254
-05-
03-2
11C
81 8281
15C
8216
C96
MO
96 M
OA
LLA
LL0.
66IN
TER
NA
L - D
ETA
ILE
D: F
ront
Spa
r, O
ne P
iece
Do
a D
etai
led
Insp
ectio
n of
the
Fron
t Spa
r, O
ne P
iece
, STA
13
07 (M
D-8
7, S
TA 1
098)
, Int
erna
l Stru
ctur
e
U65
54-0
45-0
254
-05-
03-2
11C
5858
11A
5812
A72
MO
72 M
OA
LLA
LL0.
33IN
TER
NA
L - D
ETA
ILE
D: F
ront
Spa
r, S
par T
angs
Do
a D
etai
led
Insp
ectio
n of
the
Fron
t Spa
r, S
par T
angs
, STA
13
07 (M
D-8
7, S
TA 1
098)
, Int
erna
l Stru
ctur
e
U66
54-0
46-0
254
-05-
03-2
11C
81 8281
11C
8212
C96
MO
96 M
OA
LLA
LL0.
67IN
TER
NA
L - D
ETA
ILE
D: R
ear S
par,
Upp
er a
nd L
ower
Tw
o P
iece
Cap
s (P
ylon
)D
o a
Det
aile
d In
spec
tion
of th
e R
ear S
par,
Upp
er a
nd L
ower
Tw
o P
iece
Cap
s (P
ylon
), S
TA 1
380
(MD
-87,
STA
117
1),
Inte
rnal
Stru
ctur
e
U67
54-0
47-0
205
-21-
01-2
11C
5996
MO
96 M
OA
LLA
LL0.
33IN
TER
NA
L - D
ETA
ILE
D: R
ear S
par,
Upp
er a
nd L
ower
Tw
o P
iece
Cap
sD
o a
Det
aile
d In
spec
tion
of th
e R
ear S
par,
Upp
er a
nd L
ower
Tw
o P
iece
Cap
s, S
TA 1
380
(MD
-87,
STA
117
1), I
nter
nal
Stru
ctur
e
U68
54-0
48-0
254
-05-
03-2
11C
81 8296
MO
96 M
OA
LLA
LL1.
00IN
TER
NA
L - D
ETA
ILE
D: Y
oke
- For
war
d E
ngin
e M
ount
Do
a D
etai
led
Insp
ectio
n of
the
Yok
e - F
orw
ard
Eng
ine
Mou
nt,
STA
130
7 (M
D-8
7, S
TA 1
098)
, Stru
ctur
e
U69
54-0
49-0
205
-21-
01-2
11C
81 8296
MO
96 M
OA
LLA
LL0.
50IN
TER
NA
L - D
ETA
ILE
D: B
olts
, Yok
e To
Fro
nt P
ylon
Spa
rD
o a
Det
aile
d In
spec
tion
of th
e B
olts
, Yok
e To
Fro
nt P
ylon
S
par,
STA
130
7 (M
D-8
7, S
TA 1
098)
, Bol
ts R
emov
ed.
70A
TA 5
5: S
TAB
ILIZ
ERS
U71
55-0
50-0
105
-21-
01-2
10S
3072
MO
72 M
OA
LLA
LL0.
67E
XTE
RN
AL
- GE
NE
RA
L V
ISU
AL:
Hor
izon
tal S
tabi
lizer
Rea
r S
par C
aps
Do
a G
ener
al V
isua
l Ins
pect
ion
of th
e H
oriz
onta
l Sta
biliz
er R
ear
Spa
r Cap
s, S
TA X
HS
10.
3 - S
TA X
HS
14.
6, E
xter
nal S
truct
ure
U72
55-0
50-0
255
-05-
03-2
11C
33 3433
01A
3402
A96
MO
96 M
OA
LLA
LL0.
83IN
TER
NA
L - D
ETA
ILE
D: H
oriz
onta
l Sta
biliz
er R
ear S
par C
aps
Do
a D
etai
led
Insp
ectio
n of
the
Hor
izon
tal S
tabi
lizer
Rea
r Spa
r C
aps,
STA
XH
S 1
0.3
- STA
XH
S 1
4.6,
Stru
ctur
e
Rev 0 19 March 2014
3-19
MD-80 MAINTENANCE MANUAL
.
0 1 2 3 4
DC
-9-8
0SF
Mai
nten
ance
Pla
nnin
g D
ocum
ent
STR
UC
TUR
AL
MA
INTE
NA
NC
E PR
OG
RA
M
MPD
ITEM
NU
MB
ERAM
M
REF
EREN
CE
P G MZO
NE
ACC
ESS
INTE
RVA
L
THR
ES.
REP
EAT
APPL
ICAB
ILIT
Y
APL
ENG
MAN
-N
OITPIR
CSED
KSATS
RU
OH
U73
55-0
51-0
105
-21-
01-2
10S
3072
MO
72 M
OA
LLA
LL0.
67E
XTE
RN
AL
- GE
NE
RA
L V
ISU
AL:
Hor
izon
tal S
tabi
lizer
Rea
r S
par C
aps
Do
a G
ener
al V
isua
l Ins
pect
ion
of th
e H
oriz
onta
l Sta
biliz
er R
ear
Spa
r Cap
s, S
TA X
HS
14.
6 - S
TA X
HR
209
.0, E
xter
nal
Stru
ctur
e
U74
55-0
51-0
255
-05-
03-2
11C
33 3433
03A
3305
A33
07A
3309
A34
04A
3406
A34
08A
3410
A
96 M
O96
MO
ALL
ALL
0.83
INTE
RN
AL
- DE
TAIL
ED
: Hor
izon
tal S
tabi
lizer
Rea
r Spa
r Cap
sD
o a
Det
aile
d In
spec
tion
of th
e H
oriz
onta
l Sta
biliz
er R
ear S
par
Cap
s, S
TA X
HS
14.
6 - S
TA X
HR
209
.0, S
truct
ure
U75
55-0
52-0
255
-05-
03-2
11C
39N
OTE
48 M
O48
MO
ALL
ALL
0.17
INTE
RN
AL
- DE
TAIL
ED
: Hor
izon
tal S
tabi
lizer
Rea
r Spa
r -
Cen
ter B
ox C
aps
Do
a D
etai
led
Insp
ectio
n of
the
Hor
izon
tal S
tabi
lizer
Rea
r Spa
r -
Cen
ter B
ox C
aps,
STA
XH
27
Left
- STA
XH
27
Rig
ht, I
nter
nal
Stru
ctur
e
AC
CE
SS
NO
TE: P
eel b
ack
and/
or re
mov
e lin
ing
and/
or
insu
latio
n as
requ
ired.
U76
55-0
53-0
255
-05-
03-2
11C
3937
03A
3705
A38
04A
3806
A
48 M
O48
MO
ALL
ALL
0.50
INTE
RN
AL
- DE
TAIL
ED
: Hor
izon
tal S
tabi
lizer
Cen
ter B
ox
Join
tsD
o a
Det
aile
d In
spec
tion
of th
e H
oriz
onta
l Sta
biliz
er C
ente
r Box
Jo
ints
, STA
XH
7.0
- S
TA X
H 2
6.0
(Lef
t&R
ight
), In
tern
al
Stru
ctur
e in
clud
es J
acks
crew
Lug
Atta
ch A
rea
U77
55-0
54-0
255
-05-
03-2
11C
3931
07C
3208
CN
OTE
48 M
O48
MO
ALL
ALL
0.42
INTE
RN
AL
- DE
TAIL
ED
: Hor
izon
tal S
tabi
lizer
Ope
ratin
g B
ulkh
ead
Join
tsD
o a
Det
aile
d In
spec
tion
of th
e Jo
ints
, Ope
ratin
g B
ulkh
ead,
S
TA L
H 9
- R
H 9
, Int
erna
l Stru
ctur
e
AC
CE
SS
NO
TE: P
eel b
ack
and/
or re
mov
e lin
ing
and/
or
insu
latio
n as
requ
ired.
U78
55-0
55-0
255
-05-
03-2
11C
30N
OTE
96 M
O96
MO
ALL
ALL
0.67
EXT
ER
NA
L - D
ETA
ILE
D: H
oriz
onta
l Sta
biliz
er U
pper
Pla
tes
Do
a D
etai
led
Insp
ectio
n of
the
Hor
izon
tal S
tabi
lizer
Upp
er
Pla
tes,
STA
XH
7.2
- S
TA X
H 2
7.2,
Ext
erna
l Stru
ctur
e
AC
CE
SS
NO
TE: P
eel b
ack
and/
or re
mov
e lin
ing
and/
or
insu
latio
n as
requ
ired.
Rev 0 19 March 2014
3-20
MD-80 MAINTENANCE MANUAL
0 1 2 3 4
DC
-9-8
0SF
Mai
nten
ance
Pla
nnin
g D
ocum
ent
STR
UC
TUR
AL
MA
INTE
NA
NC
E PR
OG
RA
M
MPD
ITEM
NU
MB
ERAM
M
REF
EREN
CE
P G MZO
NE
ACC
ESS
INTE
RVA
L
THR
ES.
REP
EAT
APPL
ICAB
ILIT
Y
APL
ENG
MAN
-N
OITPIR
CSED
KSATS
RU
OH
U79
55-0
56-0
255
-05-
03-2
11C
3096
MO
96 M
OA
LLA
LL0.
67E
XTE
RN
AL
- DE
TAIL
ED
: Hor
izon
tal S
tabi
lizer
Upp
er P
late
sD
o a
Det
aile
d In
spec
tion
of th
e H
oriz
onta
l Sta
biliz
er U
pper
P
late
s, S
TA X
H 2
7.2
- STA
XH
R 2
09, E
xter
nal S
truct
ure
U80
55-0
57-0
255
-05-
03-2
11C
35 36N
OTE
96 M
O96
MO
ALL
ALL
1.00
INTE
RN
AL
- DE
TAIL
ED
: Ele
vato
r Spa
r Cap
sD
o a
Det
aile
d In
spec
tion
of th
e E
leva
tor S
par C
aps,
STA
XE
3.
4 - S
TA X
E 2
36.0
, Int
erna
l Stru
ctur
e
AC
CE
SS
NO
TE: R
emov
e le
adin
g ed
ge.
U81
55-0
58-0
255
-05-
03-2
11C
3096
MO
96 M
OA
LLA
LL0.
76E
XTE
RN
AL
- DE
TAIL
ED
: Ele
vato
r Upp
er a
nd L
ower
Ski
n P
anel
sD
o a
Det
aile
d In
spec
tion
of th
e E
leva
tor U
pper
and
Low
er S
kin
Pan
els,
STA
XE
3.4
- S
TA X
E 2
36.0
, Ext
erna
l Stru
ctur
e
U82
55-0
59-0
255
-05-
03-2
11C
3096
MO
96 M
OA
LLA
LL0.
76E
XTE
RN
AL
- DE
TAIL
ED
: Ele
vato
r Ant
i Flo
at T
ab, G
eare
d an
d C
ontro
l Tab
sD
o a
Det
aile
d In
spec
tion
of th
e E
leva
tor A
nti F
loat
Tab
, Gea
red
and
Con
trol T
abs,
STA
XE
171
.0 -
STA
XE
228
.0, S
truct
ure
U83
55-0
59-0
305
-21-
01-2
80S
3072
MO
72 M
OAL
LAL
L0.
42EX
TER
NA
L - S
PEC
IAL
DE
TAIL
ED: A
nti F
loat
Tab
, Gea
red
and
Con
trol T
abs,
(Hon
eyco
mb
Stru
ctur
e)D
o a
Spe
cial
Det
aile
d In
spec
tion
of th
e A
nti F
loat
Tab
, Gea
red
and
Con
trol T
abs
(Hon
eyco
mb
Stru
ctur
e), S
TA X
E 1
71.0
- S
TA
XE 2
28.0
,Tap
Test
for d
elam
inat
ion
with
met
al s
kin
U84
55-0
60-0
255
-05-
03-2
11C
5996
MO
96 M
OA
LLA
LL0.
34E
XTE
RN
AL
- DE
TAIL
ED
: Ver
tical
Sta
biliz
er F
ront
Spa
r (A
ttach
men
t Tan
gs)
Do
a D
etai
led
Insp
ectio
n of
the
Ver
tical
Sta
biliz
er F
ront
Spa
r (A
ttach
men
t Tan
gs),
STA
138
8 (M
D-8
7, S
TA 1
179)
, Stru
ctur
e
U85
55-0
61-0
255
-05-
03-2
11C
6196
MO
96 M
OA
LLA
LL0.
67E
XTE
RN
AL
- DE
TAIL
ED
: Ver
tical
Sta
biliz
er R
ear S
par
(Atta
chm
ent T
angs
)D
o a
Det
aile
d In
spec
tion
of th
e V
ertic
al S
tabi
lizer
Rea
r Spa
r (A
ttach
men
t Tan
gs),
STA
146
3 (M
D-8
7, S
TA 1
254)
, Stru
ctur
e
U86
55-0
62-0
255
-05-
03-2
11C
63 6496
MO
96 M
OA
LLA
LL0.
75IN
TER
NA
L - D
ETA
ILE
D: V
ertic
al S
tabi
lizer
Fro
nt S
par
Do
a D
etai
led
Insp
ectio
n of
the
Ver
tical
Sta
biliz
er F
ront
Spa
r, S
TA Z
FS 4
.7 -
STA
ZFS
154
.8, F
orw
ard
and
Aft
Face
Stru
ctur
e
Rev 0 19 March 2014
3-21
MD-80 MAINTENANCE MANUAL
0 1 2 3 4
DC
-9-8
0SF
Mai
nten
ance
Pla
nnin
g D
ocum
ent
STR
UC
TUR
AL
MA
INTE
NA
NC
E PR
OG
RA
M
MPD
ITEM
NU
MB
ERAM
M
REF
EREN
CE
P G MZO
NE
ACC
ESS
INTE
RVA
L
THR
ES.
REP
EAT
APPL
ICAB
ILIT
Y
APL
ENG
MAN
-N
OITPIR
CSED
KSATS
RU
OH
U87
55-0
63-0
155
-05-
03-2
11C
64 6564
03A
6404
A64
05A
6406
A64
07A
6408
A
96 M
O96
MO
ALL
ALL
0.40
INTE
RN
AL
- DE
TAIL
ED
: Ver
tical
Sta
biliz
er R
ear S
par
Do
a D
etai
led
Insp
ectio
n of
the
Ver
tical
Sta
biliz
er R
ear S
par,
STA
ZR
S -5
.0 -
STA
ZR
S 1
70.0
, For
war
d an
d A
ft Fa
ce
Stru
ctur
e
U88
55-0
64-0
155
-05-
03-2
11C
6096
MO
96 M
OA
LLA
LL0.
34E
XTE
RN
AL
- DE
TAIL
ED
: Atta
chm
ent,
Rud
der S
par C
aps
Do
a D
etai
led
Insp
ectio
n of
the
Rud
der S
par C
aps
Atta
chm
ent,
STA
ZR
10.
0 - S
TA Z
R 1
65, E
xter
nal S
truct
ure
U89
55-0
64-0
305
-21-
01-2
80F
6015
000
FC15
000
FCAL
LAL
L0.
75EX
TER
NA
L - S
PEC
IAL
DET
AILE
D: R
udde
r Spa
r Cap
sD
o a
Spe
cial
Det
aile
d In
spec
tion
of th
e R
udde
r Spa
r Cap
s,
STA
ZR
10.
0 - S
TA Z
R 1
65, T
apTe
st fo
r Del
amin
atio
n on
C
ompo
site
(Ext
erna
l)
U90
55-0
64-0
405
-21-
01-2
80F
6530
000
FC30
000
FCAL
LAL
L1.
00IN
TER
NAL
- SP
ECIA
L D
ETAI
LED
: Rud
der S
par C
aps
Do
a S
peci
al D
etai
led
Insp
ectio
n of
the
Rud
der S
par C
aps,
S
TA Z
R 1
0.0
- STA
ZR
165
, N.D
.T. I
nspe
ctio
n, M
etal
(Int
erna
l)
U91
55-0
65-0
255
-05-
03-2
11C
6096
MO
96 M
OA
LLA
LL0.
83E
XTE
RN
AL
- DE
TAIL
ED
: Rud
der S
kin
Pan
els
Do
a D
etai
led
Insp
ectio
n of
the
Rud
der S
kin
Pan
els,
STA
ZR
8.
0 - S
TA Z
R 1
79.0
, Ext
erna
l Stru
ctur
e
U92
55-0
66-0
255
-05-
03-2
11C
3963
06A
48 M
O48
MO
ALL
ALL
0.83
EXT
ER
NA
L - D
ETA
ILE
D: H
oriz
onta
l Sta
biliz
er P
ivot
Sup
port
Fitti
ngs
Do
a D
etai
led
Insp
ectio
n of
the
Hor
izon
tal S
tabi
lizer
Piv
ot
Sup
port
Fitti
ngs,
STA
XH
7.2
(Lef
t&R
ight
)&S
TA Z
RS
173
.0,
Stru
ctur
e
U93
55-0
67-0
255
-05-
03-2
11C
35 3696
MO
96 M
OA
LLA
LL0.
67IN
TER
NA
L - D
ETA
ILE
D: E
leva
tor A
ssem
bly
Hin
ges
Do
a D
etai
led
Insp
ectio
n of
the
Ele
vato
r Ass
embl
y H
inge
s -
STA
's X
E 2
, 49,
103
, 157
, 204
, 225
, Stru
ctur
e
U94
55-1
63-0
105
-21-
01-2
10F
6015
000
FC15
000
FCA
LLA
LL0.
17E
XTE
RN
AL
- GE
NE
RA
L V
ISU
AL:
Ver
tical
Sta
biliz
er S
kin
Pan
els,
Lea
ding
Edg
e&Ti
p C
apD
o a
Gen
eral
Vis
ual I
nspe
ctio
n of
the
Ver
tical
Sta
biliz
er S
kin
Pan
els,
Lea
ding
Edg
e&Ti
p C
ap, E
xter
nal S
truct
ure
U95
55-1
63-0
255
-05-
03-2
11C
6464
04A
6405
A64
06A
6407
A64
08A
96 M
O96
MO
ALL
ALL
0.34
INTE
RN
AL
- DE
TAIL
ED
: Ver
tical
Sta
biliz
er S
kin
Pan
els,
Le
adin
g E
dge&
Tip
Cap
Do
a D
etai
led
Insp
ectio
n of
the
Ver
tical
Sta
biliz
er S
kin
Pan
els,
Le
adin
g E
dge&
Tip
Cap
, Int
erna
l Stru
ctur
e
96A
TA 5
7: W
ING
S
Rev 0 19 March 2014
3-22
MD-80 MAINTENANCE MANUAL
0 1 2 3 4
DC
-9-8
0SF
Mai
nten
ance
Pla
nnin
g D
ocum
ent
STR
UC
TUR
AL
MA
INTE
NA
NC
E PR
OG
RA
M
MPD
ITEM
NU
MB
ERAM
M
REF
EREN
CE
P G MZO
NE
ACC
ESS
INTE
RVA
L
THR
ES.
REP
EAT
APPL
ICAB
ILIT
Y
APL
ENG
MAN
-N
OITPIR
CSED
KSATS
RU
OH
U97
57-0
68-0
257
-05-
03-2
11C
15 1615
79C
1679
C72
MO
72 M
OA
LLA
LL0.
67IN
TER
NA
L - D
ETA
ILE
D: O
uter
Win
g R
ear S
par W
ebD
o a
Det
aile
d In
spec
tion
of th
e O
uter
Win
g R
ear S
par W
eb,
STA
XC
W 1
21.6
, Stru
ctur
e
U98
57-0
69-0
257
-05-
03-2
11C
13 1413
35C
1436
C72
MO
72 M
OA
LLA
LL0.
50IN
TER
NA
L - D
ETA
ILE
D: O
uter
Win
g, L
ower
Tee
Cap
at
Bul
khea
d, S
TA X
CW
121
.6D
o a
Det
aile
d In
spec
tion
of th
e Lo
wer
Tee
Cap
at B
ulkh
ead,
S
TA X
CW
121
.6, S
truct
ure
U99
57-0
70-0
105
-21-
01-2
10F
13 1411
60C
1263
C30
000
FC30
000
FCA
LLA
LL0.
33IN
TER
NA
L - G
EN
ER
AL
VIS
UA
L: O
uter
Win
g B
ulkh
ead
XCW
12
1.5
at F
ront
Spa
r Jac
k P
oint
Do
a G
ener
al V
isua
l Ins
pect
ion
of th
e O
uter
Win
g B
ulkh
ead
XCW
121
.5 a
t Fro
nt S
par J
ack
Poi
nt, I
nter
nal S
truct
ure
U10
0
57-0
70-0
257
-05-
03-2
11C
11 1296
MO
96 M
OA
LLA
LL0.
83E
XTE
RN
AL
- DE
TAIL
ED
: Bul
khea
d XC
W 1
21.5
at F
ront
Spa
r Ja
ck P
oint
Do
a D
etai
led
Insp
ectio
n of
the
Bul
khea
d XC
W 1
21.5
at F
ront
S
par J
ack
Poi
nt, E
xter
nal S
truct
ure
U10
1
57-0
71-0
257
-05-
03-2
11C
11 1296
MO
96 M
OA
LLA
LL2.
50IN
TER
NA
L - D
ETA
ILE
D: S
lat T
rack
Cut
outs
Do
a D
etai
led
Insp
ectio
n of
the
Sla
t Tra
ck C
utou
ts, S
TA X
IS
12.3
- S
TA X
OS
610
.3, I
nter
nal S
truct
ure
U10
2
57-0
72-0
205
-21-
01-2
11C
15 1672
MO
72 M
OA
LLA
LL0.
67IN
TER
NA
L - D
ETA
ILE
D: O
uter
Win
g R
ear S
par
Do
a D
etai
led
Insp
ectio
n of
the
Win
g R
ear S
par (
Out
boar
d),
STA
XC
W 1
21.6
- S
TA X
W 5
36.8
, Aft
Face
Rev 0 19 March 2014
3-23
MD-80 MAINTENANCE MANUAL
0 1 2 3 4
DC
-9-8
0SF
Mai
nten
ance
Pla
nnin
g D
ocum
ent
STR
UC
TUR
AL
MA
INTE
NA
NC
E PR
OG
RA
M
MPD
ITEM
NU
MB
ERAM
M
REF
EREN
CE
P G MZO
NE
ACC
ESS
INTE
RVA
L
THR
ES.
REP
EAT
APPL
ICAB
ILIT
Y
APL
ENG
MAN
-N
OITPIR
CSED
KSATS
RU
OH
U10
3
57-0
72-0
357
-05-
03-2
11C
13 1413
55C
1357
C13
61C
1363
C13
65C
1367
C13
71C
1373
C13
77C
1379
C14
54C
1456
C14
60C
1462
C14
64C
1466
C14
70C
1472
C14
76C
1478
C
120
MO
120
MO
ALL
ALL
0.67
INTE
RN
AL
- DE
TAIL
ED
: Out
er W
ing
Rea
r Spa
rD
o a
Det
aile
d In
spec
tion
of th
e W
ing
Rea
r Spa
r (O
utbo
ard)
, S
TA X
CW
121
.6 -
STA
XW
536
.8, F
orw
ard
Face
U10
4
57-0
73-0
257
-05-
03-2
11C
21 2221
04C
2105
C21
10C
2116
C22
04C
2205
C22
10C
2216
C
96 M
O96
MO
ALL
ALL
0.67
INTE
RN
AL
- DE
TAIL
ED
: Atta
ch A
ngle
(Top
Win
g To
Cen
ter
Fuse
lage
)D
o a
Det
aile
d In
spec
tion
of th
e A
ttach
Ang
le (T
op W
ing
To
Cen
ter F
usel
age)
, STA
811
- 92
7 (M
D-8
7, S
TA 6
97 -
813)
, S
truct
ure,
Fill
et re
mov
ed
U10
5
57-0
74-0
257
-05-
03-2
11C
2323
01C
2302
C96
MO
96 M
OA
LLA
LL0.
50IN
TER
NA
L - D
ETA
ILE
D: C
ente
r Win
g R
ear S
par W
ebD
o a
Det
aile
d In
spec
tion
of th
e C
ente
r Win
g R
ear S
par W
eb,
STA
XC
W 5
8.6
Left
To X
CW
58.
6 R
ight
, For
war
d Fa
ce
U10
6
57-0
74-0
305
-21-
01-2
11S
55 5672
MO
72 M
OA
LLA
LL0.
50E
XTE
RN
AL
- DE
TAIL
ED
: Cen
ter W
ing
Rea
r Spa
r Web
Do
a D
etai
led
Insp
ectio
n of
the
Cen
ter W
ing
Rea
r Spa
r Web
, S
TA X
CW
58.
6 Le
ft To
XC
W 5
8.6
Rig
ht, E
xter
nal S
truct
ure
U10
7
57-0
75-0
257
-05-
03-2
11C
2313
35C
1436
C72
MO
72 M
OA
LLA
LL0.
67IN
TER
NA
L - D
ETA
ILE
D: C
ente
r Win
g R
ear S
par W
ebD
o a
Det
aile
d In
spec
tion
of th
e R
ear S
par W
eb, S
TA X
CW
58.
6 - X
CW
121
.6 (L
eft&
Rig
ht),
Forw
ard
Face
Rev 0 19 March 2014
3-24
MD-80 MAINTENANCE MANUAL
0 1 2 3 4
DC
-9-8
0SF
Mai
nten
ance
Pla
nnin
g D
ocum
ent
STR
UC
TUR
AL
MA
INTE
NA
NC
E PR
OG
RA
M
MPD
ITEM
NU
MB
ERAM
M
REF
EREN
CE
P G MZO
NE
ACC
ESS
INTE
RVA
L
THR
ES.
REP
EAT
APPL
ICAB
ILIT
Y
APL
ENG
MAN
-N
OITPIR
CSED
KSATS
RU
OH
U10
8
57-0
75-0
305
-21-
01-2
11S
15 1672
MO
72 M
OA
LLA
LL0.
23E
XTE
RN
AL
- DE
TAIL
ED
: Cen
ter W
ing
Rea
r Spa
r Web
Do
a D
etai
led
Insp
ectio
n of
the
Cen
ter W
ing
Rea
r Spa
r Web
, S
TA X
CW
58.
6 - X
CW
121
.6 (L
eft&
Rig
ht),
Ext
erna
l Stru
ctur
e
U10
9
57-0
76-0
205
-21-
01-2
10C
13 1413
35C
1436
C15
79C
1679
C
72 M
O72
MO
ALL
ALL
0.33
INTE
RN
AL
- GE
NE
RA
L V
ISU
AL:
Win
g U
pper
Rea
r Spa
r Cap
Do
a G
ener
al V
isua
l Ins
pect
ion
of th
e W
ing
Upp
er R
ear S
par
Cap
(Dog
Leg
), S
TA X
CW
79.
0 - S
TA X
RS
111
.0, F
orw
ard
Face
U11
0
57-0
76-0
357
-05-
03-2
11S
15 1672
MO
72 M
OA
LLA
LL0.
27E
XTE
RN
AL
- DE
TAIL
ED
: Win
g U
pper
Rea
r Spa
r Cap
(Dog
Le
g)D
o a
Det
aile
d In
spec
tion
of th
e W
ing
Upp
er R
ear S
par C
ap
(Dog
Leg
), S
TA X
CW
79.
0 - S
TA X
RS
111
.0, E
xter
nal S
truct
ure
U11
1
57-0
77-0
257
-05-
03-2
11C
55 5672
MO
72 M
OA
LLA
LL0.
33IN
TER
NA
L - D
ETA
ILE
D: C
ente
r Win
g R
ear S
par F
ittin
gD
o a
Det
aile
d In
spec
tion
of th
e C
ente
r Win
g R
ear S
par F
ittin
g,
STA
XC
W 5
8.6
at tr
ap P
anel
/Rea
r Spa
r Int
erse
ctio
n, S
truct
ure
U11
2
57-0
78-0
257
-05-
03-2
11C
11 1296
MO
96 M
OA
LLA
LL0.
50IN
TER
NA
L - D
ETA
ILE
D: C
ente
r Win
g Fr
ont S
par C
ap S
plic
eD
o a
Det
aile
d In
spec
tion
of th
e C
ente
r Win
g Fr
ont S
par C
ap
Spl
ice,
STA
XC
W 9
2.0,
Stru
ctur
e
U11
3
57-0
79-0
205
-21-
01-2
10C
5151
07C
5138
C48
MO
48 M
OA
LLA
LL0.
50IN
TER
NA
L - D
ETA
ILE
D: C
ente
r Win
g Fr
ont S
par W
ebD
o a
Det
aile
d In
spec
tion
of th
e C
ente
r Win
g Fr
ont S
par W
eb,
STA
XC
W 5
8.6
Left
- XC
W 5
8.6
Rig
ht, S
TA 8
26 (M
D-8
7, S
TA
712)
, For
war
d Fa
ce
U11
4
57-0
79-0
357
-05-
03-2
11C
2323
01C
2302
C96
MO
96 M
OA
LLA
LL0.
42IN
TER
NA
L - D
ETA
ILE
D: C
ente
r Win
g Fr
ont S
par W
ebD
o a
Det
aile
d In
spec
tion
of th
e C
ente
r Win
g Fr
ont S
par W
eb,
STA
XC
W 5
8.6
Left
- XC
W 5
8.6
Rig
ht, S
TA 8
26 (M
D-8
7, S
TA
712)
, Aft
Face
U11
5
57-0
80-0
257
-05-
03-2
11C
13 1421
04C
2105
C21
06C
2204
C22
05C
2206
C
72 M
O72
MO
ALL
ALL
0.67
INTE
RN
AL
- DE
TAIL
ED
: Out
er W
ing
Upp
er a
nd L
ower
Ski
n P
anel
Do
a D
etai
led
Insp
ectio
n of
the
Out
er W
ing
Upp
er a
nd L
ower
S
kin
Pan
el S
TA X
CW
58.
6 - X
CW
111
U11
6
57-0
80-0
357
-05-
03-2
11C
13 1412
0 M
O12
0 M
OA
LLA
LL0.
67IN
TER
NA
L - D
ETA
ILE
D: O
uter
Win
g U
pper
and
Low
er S
kin
Pan
elD
o a
Det
aile
d In
spec
tion
of th
e O
uter
Win
g U
pper
and
Low
er
Ski
n P
anel
STA
XC
W 1
11 to
Tip
of T
ank
Rev 0 19 March 2014
3-25
MD-80 MAINTENANCE MANUAL
0 1 2 3 4
DC
-9-8
0SF
Mai
nten
ance
Pla
nnin
g D
ocum
ent
STR
UC
TUR
AL
MA
INTE
NA
NC
E PR
OG
RA
M
MPD
ITEM
NU
MB
ERAM
M
REF
EREN
CE
P G MZO
NE
ACC
ESS
INTE
RVA
L
THR
ES.
REP
EAT
APPL
ICAB
ILIT
Y
APL
ENG
MAN
-N
OITPIR
CSED
KSATS
RU
OH
U11
7
57-0
81-0
257
-05-
03-2
1157
-05-
03-2
80C
1096
MO
96 M
OA
LLA
LL6.
66E
XTE
RN
AL
- DE
TAIL
ED
: Out
er W
ing
Upp
er a
nd L
ower
Ski
n P
anel
Do
a D
etai
led
Insp
ectio
n of
the
Out
er W
ing
Upp
er a
nd L
ower
S
kin
Pan
el, S
TA X
CW
70.
0 - X
W 5
60.0
Sur
face
s
U11
8
57-0
82-0
257
-05-
03-2
11C
13 1413
35C
1436
C72
MO
72 M
OA
LLA
LL1.
00IN
TER
NA
L - D
ETA
ILE
D: U
pper
Win
g D
oor C
utou
tsD
o a
Det
aile
d In
spec
tion
of th
e C
utou
ts, U
pper
Win
g D
oor,
STA
XC
W 5
8.6
- XC
W 1
11, I
nter
nal S
truct
ure
U11
9
57-0
82-0
357
-05-
03-2
11C
13 1413
03C
1307
C13
11C
1321
C13
23C
1325
C13
27C
1335
C13
37C
1339
C14
09C
1410
C14
14C
1424
C14
26C
1428
C14
30C
1436
C14
38C
1440
C
120
MO
120
MO
ALL
ALL
0.67
INTE
RN
AL
- DE
TAIL
ED
: Upp
er W
ing
Doo
r Cut
outs
Do
a D
etai
led
Insp
ectio
n of
the
Upp
er W
ing
Doo
r Cut
outs
, STA
XC
W 1
11 to
Tip
of T
ank,
Inte
rnal
Stru
ctur
e
U12
0
57-0
83-0
257
-05-
03-2
11C
1072
MO
72 M
OA
LLA
LL0.
34E
XTE
RN
AL
- DE
TAIL
ED
: Out
er W
ing
Low
er S
kin
Pan
elD
o a
Det
aile
d In
spec
tion
of th
e O
uter
Win
g Lo
wer
Ski
n P
anel
, S
TA X
CW
58.
6 - S
TA X
W 5
60.8
, Ext
erna
l Stru
ctur
e
U12
1
57-0
84-0
257
-05-
03-2
11C
2396
MO
96 M
OA
LLA
LL0.
25IN
TER
NA
L - D
ETA
ILE
D: C
ente
r Win
g U
pper
Ski
n P
anel
sD
o a
Det
aile
d In
spec
tion
of th
e C
ente
r Win
g U
pper
Ski
n P
anel
s, S
TA X
CW
121
Lef
t - S
TA X
W 1
21 R
ight
, Int
erna
l S
truct
ure
U12
2
57-0
85-0
257
-05-
03-2
11C
2323
01C
2302
C96
MO
96 M
OA
LLA
LL0.
17IN
TER
NA
L - D
ETA
ILE
D: C
ente
r Win
g U
pper
Ski
n P
anel
s, D
oor
Cut
outs
Do
a D
etai
led
Insp
ectio
n of
the
Cen
ter W
ing
Upp
er S
kin
Pan
els,
Doo
r Cut
outs
, STA
XC
W 1
21 L
eft -
STA
XC
W 1
21
Rig
ht, S
truct
ure
Rev 0 19 March 2014
3-26
MD-80 MAINTENANCE MANUAL
0 1 2 3 4
DC
-9-8
0SF
Mai
nten
ance
Pla
nnin
g D
ocum
ent
STR
UC
TUR
AL
MA
INTE
NA
NC
E PR
OG
RA
M
MPD
ITEM
NU
MB
ERAM
M
REF
EREN
CE
P G MZO
NE
ACC
ESS
INTE
RVA
L
THR
ES.
REP
EAT
APPL
ICAB
ILIT
Y
APL
ENG
MAN
-N
OITPIR
CSED
KSATS
RU
OH
U12
3
57-0
86-0
257
-05-
03-2
11C
2313
35C
1436
C23
01C
2302
C
96 M
O96
MO
ALL
ALL
0.20
INTE
RN
AL
- DE
TAIL
ED
: Cen
ter W
ing,
Low
er S
kin
Pan
elD
o a
Det
aile
d In
spec
tion
of th
e C
ente
r Win
g, L
ower
Ski
n P
anel
, S
TA X
CW
121
Lef
t - S
TA X
CW
121
Rig
ht, S
truct
ure
U12
4
57-0
87-0
257
-05-
03-2
11C
15 1672
MO
72 M
OA
LLA
LL0.
50IN
TER
NA
L - D
ETA
ILE
D: M
ain
Land
ing
Gea
r Sup
port
Fitti
ngD
o a
Det
aile
d In
spec
tion
of th
e M
ain
Land
ing
Gea
r Sup
port
Fitti
ng, ,
STA
XC
W 1
04.5
Aft
Sur
face
, Stru
ctur
e
U12
5
57-0
88-0
257
-05-
03-2
11C
15 1672
MO
72 M
OA
LLA
LL0.
53IN
TER
NA
L - D
ETA
ILE
D: A
ft Fl
ap F
lap
Hin
ges
Do
a D
etai
led
Insp
ectio
n of
the
Aft
Flap
Hin
ges,
STA
's X
RS
11
1.5,
164
.0, 2
67.0
,&35
3.0,
Stru
ctur
e
U12
6
57-0
89-0
257
-05-
03-2
11C
15 1672
MO
72 M
OA
LLA
LL0.
40IN
TER
NA
L - D
ETA
ILE
D: W
ing
Flap
Stu
dsD
o a
Det
aile
d In
spec
tion
of th
e W
ing
Flap
Stu
ds, S
TA's
XR
S
111.
5, 1
64.0
, 267
.0,&
353.
0, V
isib
le S
truct
ure
U12
7
57-0
90-0
257
-05-
03-2
11C
15 1672
MO
72 M
OA
LLA
LL0.
20IN
TER
NA
L - D
ETA
ILE
D: S
poile
r Driv
e Fi
tting
Do
a D
etai
led
Insp
ectio
n of
the
Spo
iler D
rive
Fitti
ng, S
TA S
TA
XTE
206
.0&
STA
XTE
297
.0, V
isib
le S
truct
ure
U12
8
57-0
91-0
105
-21-
01-2
10F
1015
000
FC15
000
FCA
LLA
LL0.
66E
XTE
RN
AL
- GE
NE
RA
L V
ISU
AL:
Aile
rons
Do
a G
ener
al V
isua
l Ins
pect
ion
of th
e A
ilero
ns, S
TA X
RS
383
.0
- STA
XR
S 5
09.5
, Ext
erna
l Stru
ctur
e
U12
9
57-0
91-0
205
-21-
01-2
80C
1096
MO
96 M
OA
LLA
LL0.
67E
XTE
RN
AL
- SP
EC
IAL
DE
TAIL
ED
: Aile
rons
Do
a S
peci
al D
etai
led
Insp
ectio
n of
the
Aile
rons
, STA
XR
S
383.
0 - S
TA X
RS
509
.5, T
apTe
st fo
r Del
amin
atio
n
U13
0
57-0
92-0
105
-21-
01-2
10S
1048
MO
48 M
OA
LLA
LL0.
40E
XTE
RN
AL
- GE
NE
RA
L V
ISU
AL:
Inbo
ard
Flap
sD
o a
Gen
eral
Vis
ual I
nspe
ctio
n of
the
Inbo
ard
Flap
s, S
TA X
IFI
0.7
- XIF
I 127
.3, E
xter
nal S
truct
ure
U13
1
57-0
92-0
357
-05-
03-2
11C
15 1696
MO
96 M
OA
LLA
LL0.
67IN
TER
NA
L - D
ETA
ILE
D: I
nboa
rd F
laps
Do
a D
etai
led
Insp
ectio
n of
the
Inbo
ard
Flap
s, S
TA X
IFI 0
.7 -
XIFI
127
.3, I
nter
nal S
truct
ure
U13
2
57-0
93-0
105
-21-
01-2
10S
1072
MO
72 M
OA
LLA
LL0.
27E
XTE
RN
AL
- GE
NE
RA
L V
ISU
AL:
Fla
p S
uppo
rt Fi
tting
sD
o a
Gen
eral
Vis
ual I
nspe
ctio
n of
the
Flap
Sup
port
Fitti
ngs,
S
TA's
XW
154
.0, 2
51.0
&33
3.0,
Stru
ctur
e
Rev 0 19 March 2014
3-27
MD-80 MAINTENANCE MANUAL
0 1 2 3 4
DC
-9-8
0SF
Mai
nten
ance
Pla
nnin
g D
ocum
ent
STR
UC
TUR
AL
MA
INTE
NA
NC
E PR
OG
RA
M
MPD
ITEM
NU
MB
ERAM
M
REF
EREN
CE
P G MZO
NE
ACC
ESS
INTE
RVA
L
THR
ES.
REP
EAT
APPL
ICAB
ILIT
Y
APL
ENG
MAN
-N
OITPIR
CSED
KSATS
RU
OH
U13
3
57-0
93-0
357
-05-
03-2
11C
15 1615
19C
1520
C15
34A
1535
A15
45A
1546
A16
19C
1620
C16
34A
1635
A16
45A
1646
A
72 M
O72
MO
ALL
ALL
0.80
INTE
RN
AL
- DE
TAIL
ED
: Inb
oard
Fla
p S
uppo
rt Fi
tting
sD
o a
Det
aile
d In
spec
tion
of th
e In
boar
d Fl
ap S
uppo
rt Fi
tting
s,
STA
's X
W 1
54.0
, 251
.0&
333.
0, S
truct
ure
U13
4
57-0
94-0
357
-05-
03-2
11C
1072
MO
72 M
OA
LLA
LL0.
60E
XTE
RN
AL
- DE
TAIL
ED
: Fla
p V
ane
Atta
ch B
rack
etD
o a
Det
aile
d In
spec
tion
of th
e Fl
ap V
ane
Atta
ch B
rack
et,
Stru
ctur
e
U13
5
57-0
95-0
205
-21-
01-2
80S
1072
MO
72 M
OAL
LA
LL0.
50EX
TER
NA
L - S
PEC
IAL
DE
TAIL
ED: I
nboa
rd S
poile
rsD
o a
Spe
cial
Det
aile
d In
spec
tion
of th
e S
poile
rs, I
nboa
rd, S
TA
XW 4
7.0
- STA
XW
138
.0,T
apTe
st fo
r Del
amin
atio
n
U13
6
57-0
96-0
257
-05-
03-2
11C
15 1615
77C
1578
C16
75C
1676
C
72 M
ON
OTE
72 M
ON
OTE
ALL
ALL
0.33
INTE
RN
AL
- DE
TAIL
ED
: Sup
port
Fitti
ngs/
Atta
ch S
truct
ure,
Fle
x Jo
int
Do
a D
etai
led
Insp
ectio
n of
the
Sup
port
Fitti
ngs/
Atta
ch
Stru
ctur
e, F
lex
Join
t.
INTE
RV
AL
NO
TE: W
hich
ever
Com
e Fi
rst.
Rev 0 19 March 2014
3-28
MD-80 MAINTENANCE MANUAL
Intentionally Left Blank
Rev 0 19 March 2014
4-1
MD-80 MAINTENANCE MANUAL
CHAPTER 4: ZONAL INSPECTION PROGRAM (ZIP)
4.1 Scope
The Zonal Inspection Program includes a general visual and, if required, physical check of the general con-dition and security of attachment of the accessible systems and structures items contained in defined zones. This includes checks for degradation such as chafing of tubing, loose duct supports, wiring damage, cable and pulley wear, fluid leaks, electrical bonding, general condition of fasteners, cracked, chipped, or miss-ing paint on composite structure, inadequate drainage, etc., and general corrosion, not covered in the MSG-3 system and structures analysis. The zonal inspection is not intended as a quality assurance after mainte-nance check for determining proper reassembly of systems, components, structures, or powerplants.
The Zonal program packages a number of General Visual (GV) Inspections into one or more zonal inspec-tions. The program includes any General Visual Inspection tasks required to assure security of attachment and general condition of any system or structural items within the zone.
4.2 Notes
1. Purpose
The Zonal Inspection Program serves two primary purposes:
a. To assess the general condition and security of attachment of all systems and structures items con-tained in each zone by use of adequate zonal inspection tasks.
b. To package a number of General Visual Inspection tasks generated against Maintenance Signifi-cant Items (MSIs) and Structural Significant Items (SSIs) into one or more Zonal tasks.
4.3 Notes: Main Cargo Door Modification (STC ST02434LA)
1. Scheduled maintenance tasks for the main cargo door modification can be found in Chapter 12.
4.4 Zonal Program Rules
1. The Zonal Inspection Program contains a series of tasks identified as Inspection-Zonal. This inspection is defined as:
“A visual examination of an interior or exterior area, installation or assembly to detect obvious damage, failure or irregularity. This level of inspection is made from within touching distance, unless otherwise specified. A mirror may be necessary to enhance visual access to all exposed sur-faces in the inspection area. This level of inspection is made under normally available lighting conditions such as daylight, hangar lighting, flashlight or drop-light and may require removal or opening of access panels or doors. Stands, ladders or platforms may be required to gain proximity to the area being checked.”
Adequate lighting and normal inspection aids are to be used as required, such as flashlight and/or inspec-tion mirror.
2. Internal/External, as used in the zonal inspection tasks, refers to the point from which the inspection is accomplished in relation to the zone.
3. The zonal task includes visual checks of all electrical wiring, hydraulic tubing, water/waste plumbing, pneumatic ducting, components, and fittings, brackets, etc., associated with systems as well as all visi-ble structure which are contained within the zone boundaries. The extent of the intended area of the inspection is defined by the access, if any, listed with each inspection item.
4. Whenever physically possible, the zonal inspections will be conducted within touching distance unless otherwise stated.
Rev 0 19 March 2014
4-2
MD-80 MAINTENANCE MANUAL
5. General Visual Inspections included in the zonal program are inspections that will detect obvious unsatisfactory conditions, damage, failures, irregularities/discrepancies in visible structure, systems and powerplant installations or assemblies.
6. Detailed and Special Detailed Inspections are not contained in the Zonal Inspection Program.
7. Zones which contain systems/components/installations are assigned a zonal inspection task to be per-formed at specified intervals.
8. Many systems, powerplant and structures General Visual Inspection tasks have been satisfied (pre-cluded) by zonal inspections required under the Zonal Inspection Program. These tasks are listed in Appendix G of this report.
9. Based on the operator’s access panel configuration, experience and scheduling requirements, the access requirements may be amended by the operator.
10. Excessive dust, debris, or overspray of corrosion inhibiting compounds, found during any inspection, are considered to be unsatisfactory condition possibly reducing the fire resistance of the airplane design. Cleanup of these materials should be a standard part of maintenance activity.
11. The scope and intent of what is to be inspected is based on what is visible within the zone with the specified access open. Any fairings, panels, or other items which are specified to be opened to gain access to a particular zone should also be inspected if they are not covered by a separately defined zonal task.
12. Design features for HIRF relative to GV Inspections were considered during the zonal program analy-sis.
13. The Enhanced Zonal Analysis Procedures (EZAP) included in MSG-3 Revision 2002 document per-mit appropriate attention to be given to electrical wiring installations. Thus, as well as determining zonal inspections, for zones that both contain electrical wiring and have potential for combustible materials being present an enhanced zonal analysis was performed. This enhanced zonal analysis pro-vided a means to identify applicable and effective tasks to minimize contamination and to address sig-nificant wiring installation discrepancies that may not be reliably detected through zonal inspection. These dedicated tasks are included in the Systems and Powerplant requirement chapter (Chapter 2) of this document.
Since these tasks are normally not system specific and do not have a Failure Effect Category, they have been included under ATA 20.
Rev 0 19 March 2014
4-3
MD-80 MAINTENANCE MANUAL
Figure 4-A: Zonal Maintenance Program Example Page
Rev 0 19 March 2014
4-4
MD-80 MAINTENANCE MANUAL
4.5 Task Summary Page Format
1. MPD Item Number.
Each task is given a unique MPD item number. The first and second digit is the ATA number. The rest of the numbers denote the MPD sequence number.
When a maintenance task is added by Everts and not part of the Boeing MD-80 MPD it will be identified by the three letter code TNK in the middle 3 digits of the task number.
2. AMM Reference.
Airplane Maintenance Manual procedure (Chapter, Section, Subject) which supports the MPD require-ment.
3. Zone.
The Zone identifies where the task is performed on the airplane.
4. Access.
The access panels or door numbers required to be opened when performing the task.
5. Internal.
Task intervals are specified in terms of letter checks.
6. Applicability.
Applicable Airplane Model and Engine. “NOTE” refers to an explanation under the task description.
Airplane (APL) Model:
• ALL = All Airplanes.
• NOTE = Airplane Applicability Note.
Engine (ENG):
• ALL = All Engines.
• NOTE = Engine Applicability Note.
7. Manhours.
Estimated labor hours (per airplane) required to perform the task(s). These labor hours do not include the time required to gain access, position work stands, defuel and purge fuel tanks, troubleshoot, nor correct discrepancies found while performing the task. The labor hours estimates are based on the use of skilled personnel and ready availability of required tools and equipment.
8. Task Description.
Description of the task to be performed. Applicability, Access and Interval notes are listed here to provide additional explanation for the other columns where “NOTE” is used.
Rev 0 19 March 2014
4-5
MD-80 MAINTENANCE MANUAL
0 1 2 3 4 6A
TA 3
2: L
AN
DIN
G G
EAR
U7
32-7
00-0
105
-21-
01-2
1017 18 43 47 55 56
NO
TE1
A1
AA
LLA
LL0.
47IN
TER
NA
L - Z
ON
AL
(GV
): La
ndin
g G
ear a
nd L
andi
ng G
ear
Doo
rsZo
nal I
nspe
ctio
n: In
tern
al -
Land
ing
Gea
r and
Lan
ding
Gea
r D
oors
(EZA
P)
AC
CE
SS
NO
TE: G
ear d
oors
ope
n
8A
TA 5
2: D
OO
RS
U9
52-8
00-0
105
-21-
01-2
1040 50
NO
TE2
C2
CA
LLA
LL0.
34E
XTE
RN
AL
- ZO
NA
L (G
V):
Doo
rs (P
asse
nger
/Car
go)
Zona
l Ins
pect
ion:
Ext
erna
l - D
oors
(Pas
seng
er/C
argo
)
AC
CE
SS
NO
TE: D
oors
clo
sed
U10
52-8
00-0
205
-21-
01-2
1051 57
NO
TE1
C1
CA
LLA
LL0.
25E
XTE
RN
AL
- ZO
NA
L (G
V):
Low
er C
argo
Doo
rs a
nd
Sur
roun
ding
Doo
r Jam
bsZo
nal I
nspe
ctio
n: E
xter
nal -
Low
er C
argo
Doo
rs a
nd
Sur
roun
ding
Doo
r Jam
bs
AC
CE
SS
NO
TE: D
oors
ope
n, b
arrie
r low
ered
U11
52-8
00-0
305
-21-
01-2
1046 58
NO
TE2
C2
CA
LLA
LL0.
72E
XTE
RN
AL
- ZO
NA
L (G
V):
Pas
seng
er D
oors
and
Sur
roun
ding
Ja
mbs
Zona
l Ins
pect
ion:
Ext
erna
l - P
asse
nger
Doo
rs a
nd S
urro
undi
ng
Jam
bs, I
nclu
ding
Ser
vice
Doo
rs, V
entra
l Sta
irs&
Em
erge
ncy
Exi
ts
AC
CE
SS
NO
TE: D
oors
ope
n
12A
TA 5
3: F
USE
LAG
E
U13
53-1
00-0
105
-21-
01-2
1020 40 50
1 A
1 A
ALL
ALL
0.30
EXT
ER
NA
L - Z
ON
AL
(GV
): Lo
wer
Fus
elag
eZo
nal I
nspe
ctio
n: E
xter
nal -
Low
er F
usel
age,
incl
udin
g R
adom
e an
d Lo
wer
Win
g Fi
llets
U14
53-1
00-0
205
-21-
01-2
1020
2 C
2 C
ALL
ALL
0.13
EXT
ER
NA
L - Z
ON
AL
(GV
): Fu
sela
ge to
Win
g Fi
llets
, Upp
erZo
nal I
nspe
ctio
n: E
xter
nal -
Fus
elag
e to
Win
g Fi
llets
, Upp
er
U15
53-1
00-0
305
-21-
01-2
1041
NO
TE2
C2
CA
LLA
LL0.
08IN
TER
NA
L - Z
ON
AL
(GV
): R
adom
eZo
nal I
nspe
ctio
n: In
tern
al -
Rad
ome,
STA
7 to
For
war
d Fa
ce o
f S
TA 3
7 P
ress
ure
Bul
khea
d (E
ZAP
)
AC
CE
SS
NO
TE: R
adom
e
ZON
EAC
CES
S
INTE
RVA
L
THR
ES.
REP
EAT
APPL
ICAB
ILIT
Y
APL
ENG
MAN
-N
OITPIR
CSED
KSATS
RU
OH
DC
-9-8
0SF
Mai
nten
ance
Pla
nnin
g D
ocum
ent
ZON
AL
INSP
ECTI
ON
PR
OG
RA
M
MPD
ITEM
NU
MB
ERAM
M
REF
EREN
CE
Rev 0 19 March 2014
4-6
MD-80 MAINTENANCE MANUAL
0 1 2 3 4
ZON
EAC
CES
S
INTE
RVA
L
THR
ES.
REP
EAT
APPL
ICAB
ILIT
Y
APL
ENG
MAN
-N
OITPIR
CSED
KSATS
RU
OH
DC
-9-8
0SF
Mai
nten
ance
Pla
nnin
g D
ocum
ent
ZON
AL
INSP
ECTI
ON
PR
OG
RA
M
MPD
ITEM
NU
MB
ERAM
M
REF
EREN
CE
U16
53-1
00-0
405
-21-
01-2
1042
4302
A1
C1
CA
LLA
LL0.
10IN
TER
NA
L - Z
ON
AL
(GV
): Fo
rwar
d A
cces
sory
Com
partm
ent
Zona
l Ins
pect
ion:
Inte
rnal
- Fo
rwar
d A
cces
sory
Com
partm
ent,
Aft
Face
of S
TA 3
7 to
For
war
d Fa
ce o
f STA
69
Bul
khea
d (E
ZAP
)
U17
53-1
00-0
505
-21-
01-2
1045
1 A
1 A
ALL
ALL
0.13
INTE
RN
AL
- ZO
NA
L (G
V):
Forw
ard
Pas
seng
er D
oor S
tairw
ell
Zona
l Ins
pect
ion:
Inte
rnal
- Fo
rwar
d P
asse
nger
Doo
r Sta
irwel
l w
ith s
tairs
ext
ende
d (E
ZAP
)
U18
53-1
00-0
605
-21-
01-2
1045
4508
A2
C2
CA
LLA
LL0.
10IN
TER
NA
L - Z
ON
AL
(GV
): Fo
rwar
d P
asse
nger
Doo
r Sta
irwel
lZo
nal I
nspe
ctio
n: In
tern
al -
Forw
ard
Pas
seng
er D
oor S
tairw
ell
with
sta
irs e
xten
ded,
acc
ess
thro
ugh
E&E
Com
partm
ent
U19
53-1
00-0
705
-21-
01-2
1045
4501
A1
C1
CA
LLAL
L0.
20IN
TER
NA
L - Z
ON
AL
(GV)
: E&E
Com
partm
ent
Zona
l Ins
pect
ion:
Inte
rnal
- E
&E
Com
partm
ent,
STA
69
to S
TA
218
(EZA
P)
U20
53-1
00-0
805
-21-
01-2
1043
NO
TE1
A1
AA
LLA
LL0.
20IN
TER
NA
L - Z
ON
AL
(GV
): N
ose
Gea
r Whe
el
Wel
l&U
npre
ssur
ized
Sid
ewal
lsZo
nal I
nspe
ctio
n: In
tern
al -
Nos
e G
ear W
heel
W
ell&
Unp
ress
uriz
ed S
idew
alls
, STA
37
to S
TA 1
10 (E
ZAP
)
AC
CE
SS
NO
TE: G
ear D
oors
Ope
n
U21
53-1
00-0
905
-21-
01-2
1051
NO
TE1
A1
AA
LLA
LL0.
20IN
TER
NA
L - Z
ON
AL
(GV
): Fo
rwar
d&C
ente
r Car
go
Com
partm
ent
Zona
l Ins
pect
ion:
Inte
rnal
- Fo
rwar
d&C
ente
r Car
go
Com
partm
ent w
ith li
ners
inst
alle
d
AC
CE
SS
NO
TE: C
argo
Com
partm
ent D
oor O
pen
U22
53-1
00-1
005
-21-
01-2
1051
NO
TE4
C4
CA
LLA
LL0.
80IN
TER
NA
L - Z
ON
AL
(GV
): Fo
rwar
d&C
ente
r Car
go
Com
partm
ent
Zona
l Ins
pect
ion:
Inte
rnal
- Fo
rwar
d&C
ente
r Car
go
Com
partm
ent,
Incl
udin
g C
eilin
g A
rea,
Lef
t&R
ight
Tun
nels
(E
ZAP
)
AC
CE
SS
NO
TE: C
argo
com
partm
ent c
eilin
g, s
idew
all l
iner
s an
d flo
or p
anel
s re
mov
ed.
Rev 0 19 March 2014
4-7
MD-80 MAINTENANCE MANUAL
0 1 2 3 4
ZON
EAC
CES
S
INTE
RVA
L
THR
ES.
REP
EAT
APPL
ICAB
ILIT
Y
APL
ENG
MAN
-N
OITPIR
CSED
KSATS
RU
OH
DC
-9-8
0SF
Mai
nten
ance
Pla
nnin
g D
ocum
ent
ZON
AL
INSP
ECTI
ON
PR
OG
RA
M
MPD
ITEM
NU
MB
ERAM
M
REF
EREN
CE
U23
53-1
00-1
105
-21-
01-2
1053
NO
TE4
C4
CA
LLA
LL0.
20IN
TER
NA
L - Z
ON
AL
(GV
): A
rea
betw
een
Low
er S
urfa
ce o
f C
abin
Flo
or to
Upp
er S
urfa
ce o
f Cen
ter W
ing
Zona
l Ins
pect
ion:
Inte
rnal
- A
rea
betw
een
Low
er S
urfa
ce o
f C
abin
Flo
or to
Upp
er S
urfa
ce o
f Cen
ter W
ing,
STA
821
to S
TA
1003
for (
MD
-81,
82,
83&
88),
STA
697
to S
TA 9
19 fo
r (M
D-8
7).
(EZA
P)
AC
CE
SS
NO
TE: F
loor
Pan
els
Rem
oved
U24
53-1
00-1
205
-21-
01-2
1023
2301
C23
02C
NO
TE
8 C
8 C
ALL
ALL
0.20
INTE
RN
AL
- ZO
NA
L (G
V):
Cen
ter W
ing
Sec
tion
Zona
l Ins
pect
ion:
Inte
rnal
- C
ente
r Win
g S
ectio
n, S
TA 8
21 to
S
TA 9
37 (M
D-8
1, 8
2, 8
3&88
)&S
TA 6
97 to
STA
823
for M
D-8
7 (E
ZAP
)
AC
CE
SS
NO
TE: F
loor
Pan
els
Rem
oved
U25
53-1
00-1
305
-21-
01-2
1054
NO
TE8
C8
CA
LLA
LL0.
20IN
TER
NA
L - Z
ON
AL
(GV
): A
rea
belo
w C
ente
r Win
g S
ectio
nZo
nal I
nspe
ctio
n: In
tern
al -
Are
a be
low
Cen
ter W
ing
Sec
tion
AC
CE
SS
NO
TE: F
illet
s R
emov
ed
U26
53-1
00-1
405
-21-
01-2
1054 55 56
NO
TE1
A1
AA
LLA
LL0.
20IN
TER
NA
L - Z
ON
AL
(GV
): L/
H&
R/H
Mai
n G
ear W
heel
Wel
lsZo
nal I
nspe
ctio
n: In
tern
al -
L/H
&R
/H M
ain
Gea
r Whe
el W
ells
an
d vi
ew Z
one
54 fr
om W
heel
Wel
ls (E
ZAP
)
AC
CE
SS
NO
TE: G
ear D
oors
Ope
n
U27
53-1
00-1
505
-21-
01-2
1057
NO
TE1
A1
AA
LLA
LL0.
10IN
TER
NA
L - Z
ON
AL
(GV
): A
ft C
argo
Com
partm
ent
Zona
l Ins
pect
ion:
Inte
rnal
- A
ft C
argo
Com
partm
ent,
STA
100
3 to
STA
133
8
AC
CE
SS
NO
TE: C
argo
Com
partm
ent D
oor O
pen
U28
53-1
00-1
605
-21-
01-2
1057
5703
C57
18C
2 C
2 C
ALL
ALL
0.08
INTE
RN
AL
- ZO
NA
L (G
V):
Aft
Car
go C
ompa
rtmen
tZo
nal I
nspe
ctio
n: In
tern
al -
Aft
Car
go C
ompa
rtmen
t (A
ft A
rea)
(E
ZAP
)
U29
53-1
00-1
705
-21-
01-2
1057
NO
TE4
C4
CA
LLA
LL0.
27IN
TER
NA
L - Z
ON
AL
(GV
): A
ft C
argo
Com
partm
ent
Zona
l Ins
pect
ion:
Inte
rnal
- A
ft C
argo
Com
partm
ent,
Incl
udin
g C
eilin
g Ar
ea, L
eft&
Rig
ht T
unne
ls (E
ZAP
)
AC
CE
SS
NO
TE: C
argo
com
partm
ent c
eilin
g an
d si
dew
all l
iner
s an
d flo
or p
anel
s re
mov
ed.
Rev 0 19 March 2014
4-8
MD-80 MAINTENANCE MANUAL
0 1 2 3 4
ZON
EAC
CES
S
INTE
RVA
L
THR
ES.
REP
EAT
APPL
ICAB
ILIT
Y
APL
ENG
MAN
-N
OITPIR
CSED
KSATS
RU
OH
DC
-9-8
0SF
Mai
nten
ance
Pla
nnin
g D
ocum
ent
ZON
AL
INSP
ECTI
ON
PR
OG
RA
M
MPD
ITEM
NU
MB
ERAM
M
REF
EREN
CE
U30
53-1
00-1
805
-21-
01-2
1051
NO
TE4
C4
CA
LLA
LL1.
00IN
TER
NA
L - Z
ON
AL
(GV
): Fo
rwar
d&C
ente
r Car
go
Com
partm
ent,
Bilg
e A
rea
Per
form
an
inte
rnal
zon
al in
spec
tion
(GV
) of t
he
Forw
ard&
Cen
ter C
argo
Com
partm
ent,
Bilg
e A
rea
(EZA
P)
AC
CE
SS
NO
TE: R
emov
e Fl
oor P
anel
s.
U31
53-1
00-1
905
-21-
01-2
1057
NO
TE4
C4
CA
LLA
LL1.
00IN
TER
NA
L - Z
ON
AL
(GV
): A
ft C
argo
Com
partm
ent,
Bilg
e A
rea
Per
form
an
inte
rnal
zon
al in
spec
tion
(GV
) of t
he A
ft C
argo
C
ompa
rtmen
t, B
ilge
Are
a (E
ZAP
)
AC
CE
SS
NO
TE: R
emov
e Fl
oor P
anel
s.
U32
53-2
00-0
105
-21-
01-2
1040 50
1 A
1 A
ALL
ALL
0.23
EXT
ER
NA
L - Z
ON
AL
(GV
): U
pper
Fus
elag
eZo
nal I
nspe
ctio
n: E
xter
nal -
Upp
er F
usel
age
-As
view
ed fr
om
grou
nd
U33
53-2
00-0
205
-21-
01-2
1040 50
2 C
2 C
ALL
ALL
0.47
EXT
ER
NA
L - Z
ON
AL
(GV
): U
pper
Fus
elag
eZo
nal I
nspe
ctio
n: E
xter
nal -
Upp
er F
usel
age
U34
53-2
00-0
305
-21-
01-2
1044
1 A
1 A
ALL
ALL
0.10
INTE
RN
AL
- ZO
NA
L (G
V):
Coc
kpit
Are
aZo
nal I
nspe
ctio
n: In
tern
al -C
ockp
it A
rea
- STA
69
- STA
160
U35
53-2
00-0
405
-21-
01-2
1044
NO
TE4
C4
CA
LLA
LL0.
30IN
TER
NA
L - Z
ON
AL
(GV
): C
ockp
it A
rea
Zona
l Ins
pect
ion:
Inte
rnal
- C
ockp
it A
rea,
- S
TA 6
9 - S
TA 1
60
(EZA
P)
AC
CE
SS
NO
TE: A
ll Pa
nels
Rem
oved
(Inc
ludi
ng
Floo
r&In
stru
men
t)
U36
53-2
00-0
505
-21-
01-2
1046 58
1 A
1 A
ALL
ALL
0.25
INTE
RN
AL
- ZO
NA
L (G
V):
Forw
ard,
Mid
and
Aft
Cab
in A
rea
Zona
l Ins
pect
ion:
Inte
rnal
- Fo
rwar
d, M
id a
nd A
ft C
abin
Are
a
U37
53-2
00-0
605
-21-
01-2
1046 58
NO
TE8
C8
CA
LLA
LL0.
50IN
TER
NA
L - Z
ON
AL
(GV
): Fo
rwar
d, M
id a
nd A
ft C
abin
Are
aZo
nal I
nspe
ctio
n: In
tern
al -
Forw
ard,
Mid
and
Aft
Cab
in A
rea
(EZA
P)
AC
CE
SS
NO
TE: C
eilin
g P
anel
s R
emov
ed
U38
53-3
00-0
105
-21-
01-2
1030 50 60
1 A
1 A
ALL
ALL
0.30
EXT
ER
NA
L - Z
ON
AL
(GV
): A
ft Fu
sela
ge&
Em
penn
age
Zona
l Ins
pect
ion:
Ext
erna
l - A
ft Fu
sela
ge&
Em
penn
age
- As
view
ed fr
om g
roun
d
Rev 0 19 March 2014
4-9
MD-80 MAINTENANCE MANUAL
0 1 2 3 4
ZON
EAC
CES
S
INTE
RVA
L
THR
ES.
REP
EAT
APPL
ICAB
ILIT
Y
APL
ENG
MAN
-N
OITPIR
CSED
KSATS
RU
OH
DC
-9-8
0SF
Mai
nten
ance
Pla
nnin
g D
ocum
ent
ZON
AL
INSP
ECTI
ON
PR
OG
RA
M
MPD
ITEM
NU
MB
ERAM
M
REF
EREN
CE
U39
53-3
00-0
205
-21-
01-2
1030 50 60
2 C
2 C
ALL
ALL
0.57
EXT
ER
NA
L - Z
ON
AL
(GV
): A
ft Fu
sela
ge&
Em
penn
age
Zona
l Ins
pect
ion:
Ext
erna
l - A
ft Fu
sela
ge&
Em
penn
age
U40
53-3
00-0
305
-21-
01-2
1059 61
NO
TE1
C1
CA
LLA
LL0.
17IN
TER
NA
L - Z
ON
AL
(GV
): A
ft Fu
sela
geZo
nal I
nspe
ctio
n: In
tern
al -
Aft
Fuse
lage
- S
TA 1
338
to S
TA
1633
(EZA
P)
AC
CE
SS
NO
TE: A
ft C
abin
Bul
khea
d D
oor
U41
53-3
00-0
405
-21-
01-2
1059
1 A
1 A
ALL
ALL
0.10
INTE
RN
AL
- ZO
NA
L (G
V):
AP
U C
ompa
rtmen
tZo
nal I
nspe
ctio
n: In
tern
al -A
PU
Com
partm
ent (
EZA
P)
42A
TA 5
5: S
TAB
ILIZ
ERS
U43
55-3
00-0
505
-21-
01-2
1031 32
NO
TE4
C4
CA
LLA
LL0.
17IN
TER
NA
L - Z
ON
AL
(GV
): H
oriz
onta
l Sta
biliz
er L
eadi
ng E
dge
Zona
l Ins
pect
ion:
Inte
rnal
-Hor
izon
tal S
tabi
lizer
Lea
ding
Edg
e (E
ZAP
)
AC
CE
SS
NO
TE: L
eadi
ng E
dge
Rem
oved
U44
55-3
00-0
605
-21-
01-2
1035 36
NO
TE4
C4
CA
LLA
LL0.
20IN
TER
NA
L - Z
ON
AL
(GV
): H
oriz
onta
l Sta
biliz
er T
raili
ng E
dge
Zona
l Ins
pect
ion:
Inte
rnal
-Hor
izon
tal S
tabi
lizer
Tra
iling
Edg
e (E
ZAP
)
AC
CE
SS
NO
TE: H
inge
d P
anel
s Lo
wer
ed
U45
55-3
00-0
705
-21-
01-2
1037 38 39 63
3705
A38
06A
6103
A63
03C
6307
C63
13C
6314
E63
19C
6320
E
4 C
4 C
ALL
ALL
0.50
INTE
RN
AL
- ZO
NA
L (G
V):
Ver
tical
Sta
biliz
er L
eadi
ng E
dge,
Tip
Fa
iring
, Rud
der a
nd A
rea
Enc
lose
d by
Fille
t Fai
ring
Zona
l Ins
pect
ion:
Inte
rnal
-Ver
tical
Sta
biliz
er L
eadi
ng E
dge,
Tip
Fa
iring
, Rud
der a
nd A
rea
Enc
lose
d by
Fille
t Fai
ring
(EZA
P)
Rev 0 19 March 2014
4-10
MD-80 MAINTENANCE MANUAL
0 1 2 3 4
ZON
EAC
CES
S
INTE
RVA
L
THR
ES.
REP
EAT
APPL
ICAB
ILIT
Y
APL
ENG
MAN
-N
OITPIR
CSED
KSATS
RU
OH
DC
-9-8
0SF
Mai
nten
ance
Pla
nnin
g D
ocum
ent
ZON
AL
INSP
ECTI
ON
PR
OG
RA
M
MPD
ITEM
NU
MB
ERAM
M
REF
EREN
CE
U46
55-3
00-0
805
-21-
01-2
1033 34
3301
A33
03A
3305
A33
07A
3309
A33
29A
3402
A34
04A
3406
A34
08A
3410
A34
30A
4 C
4 C
ALL
ALL
1.00
INTE
RN
AL
- ZO
NA
L (G
V):
Hor
izon
tal S
tabi
lizer
Inte
rspa
r Box
in
clud
ing
Tip
Per
form
an
inte
rnal
zon
al in
spec
tion
(GV
) of t
he le
ft an
d rig
ht
horiz
onta
l sta
biliz
er in
ters
par b
ox in
clud
ing
tip.
47A
TA 5
7: W
ING
S
U48
57-5
00-0
105
-21-
01-2
1010
NO
TE1
A1
AA
LLA
LL0.
10E
XTE
RN
AL
- ZO
NA
L (G
V):
Left
Win
g Lo
wer
Sur
face
Zona
l Ins
pect
ion:
Ext
erna
l - L
eft W
ing
Low
er s
urfa
ce
AC
CE
SS
NO
TE: V
iew
ed fr
om th
e gr
ound
, Sla
ts a
nd F
laps
ex
tend
ed
U49
57-5
00-0
205
-21-
01-2
1010
NO
TE2
C2
CA
LLA
LL0.
17E
XTE
RN
AL
- ZO
NA
L (G
V):
Left
Win
g U
pper
and
Low
er
Sur
face
, inc
ludi
ng a
ll fli
ght c
ontro
l sur
face
sZo
nal I
nspe
ctio
n: E
xter
nal -
Lef
t Win
g U
pper
and
low
er s
urfa
ce,
incl
udin
g al
l flig
ht c
ontro
l sur
face
s.
AC
CE
SS
NO
TE: A
ll fli
ght c
ontro
l sur
face
s in
the
exte
nded
/dep
loye
d po
sitio
n.
U50
57-5
00-0
305
-21-
01-2
1011
NO
TE1
C1
CA
LLA
LL0.
13IN
TER
NA
L - Z
ON
AL
(GV
): Le
ft W
ing
Fixe
d Le
adin
g E
dge
Com
partm
ent
Zona
l Ins
pect
ion:
Inte
rnal
- Le
ft W
ing
Fixe
d Le
adin
g E
dge
Com
partm
ent (
EZA
P)
AC
CE
SS
NO
TE: A
ll lo
wer
pan
els
rem
oved
Rev 0 19 March 2014
4-11
MD-80 MAINTENANCE MANUAL
0 1 2 3 4
ZON
EAC
CES
S
INTE
RVA
L
THR
ES.
REP
EAT
APPL
ICAB
ILIT
Y
APL
ENG
MAN
-N
OITPIR
CSED
KSATS
RU
OH
DC
-9-8
0SF
Mai
nten
ance
Pla
nnin
g D
ocum
ent
ZON
AL
INSP
ECTI
ON
PR
OG
RA
M
MPD
ITEM
NU
MB
ERAM
M
REF
EREN
CE
U51
57-5
00-0
405
-21-
01-2
1013
1355
C13
57C
1361
C13
63C
1365
C13
67C
1371
C13
73C
1377
C13
79C
NO
TE
8 C
8 C
ALL
ALL
0.34
INTE
RN
AL
- ZO
NA
L (G
V):
Left
Win
g In
ters
par B
ox S
ectio
nZo
nal I
nspe
ctio
n: In
tern
al -
Left
Win
g In
ters
par B
ox S
ectio
n (E
ZAP
)
AC
CE
SS
NO
TE: A
ll pa
nels
rem
oved
U52
57-5
00-0
505
-21-
01-2
1013
NO
TE8
C8
CA
LLA
LL0.
08IN
TER
NA
L - Z
ON
AL
(GV
): Le
ft W
ing
Ven
t Box
Zona
l Ins
pect
ion:
Inte
rnal
- Le
ft W
ing
Ven
t Box
(EZA
P)
AC
CE
SS
NO
TE: A
ll pa
nels
rem
oved
U53
57-5
00-0
605
-21-
01-2
1011
1135
A11
37A
1138
C11
39A
1146
A11
47A
4 C
4 C
ALL
ALL
0.07
INTE
RN
AL
- ZO
NA
L (G
V):
Left
Win
g Ti
p A
ssem
bly
Zona
l Ins
pect
ion:
Inte
rnal
- Le
ft W
ing
Tip
Ass
embl
y, S
TA X
w
560
U54
57-5
00-0
705
-21-
01-2
1015
NO
TE1
C1
CA
LLA
LL0.
34IN
TER
NA
L - Z
ON
AL
(GV
): Le
ft W
ing
Fixe
d Tr
ailin
g E
dge
Com
partm
ent
Zona
l Ins
pect
ion:
Inte
rnal
- Le
ft W
ing
Fixe
d Tr
ailin
g E
dge
Com
partm
ent,
incl
udin
g Fl
ap H
inge
Are
a (E
ZAP
)
AC
CE
SS
NO
TE: A
ll hi
nged
pan
els
low
ered
U55
57-6
00-0
105
-21-
01-2
1010
NO
TE1
A1
AA
LLA
LL0.
10E
XTE
RN
AL
- ZO
NA
L (G
V):
Rig
ht W
ing
Low
er S
urfa
ceZo
nal I
nspe
ctio
n: E
xter
nal -
Rig
ht W
ing
Low
er s
urfa
ce
AC
CE
SS
NO
TE: V
iew
ed fr
om th
e gr
ound
, Sla
ts a
nd F
laps
ex
tend
ed
U56
57-6
00-0
205
-21-
01-2
1010
NO
TE2
C2
CA
LLA
LL0.
17E
XTE
RN
AL
- ZO
NA
L (G
V):
Rig
ht W
ing
Upp
er a
nd L
ower
S
urfa
ce, i
nclu
ding
all
fligh
t con
trol s
urfa
ces
Zona
l Ins
pect
ion:
Ext
erna
l - R
ight
Win
g U
pper
and
low
er
surfa
ce, i
nclu
ding
all
fligh
t con
trol s
urfa
ces.
AC
CE
SS
NO
TE: A
ll fli
ght c
ontro
l sur
face
s in
the
exte
nded
/dep
loye
d po
sitio
n.
Rev 0 19 March 2014
4-12
MD-80 MAINTENANCE MANUAL
0 1 2 3 4
ZON
EAC
CES
S
INTE
RVA
L
THR
ES.
REP
EAT
APPL
ICAB
ILIT
Y
APL
ENG
MAN
-N
OITPIR
CSED
KSATS
RU
OH
DC
-9-8
0SF
Mai
nten
ance
Pla
nnin
g D
ocum
ent
ZON
AL
INSP
ECTI
ON
PR
OG
RA
M
MPD
ITEM
NU
MB
ERAM
M
REF
EREN
CE
U57
57-6
00-0
305
-21-
01-2
1012
NO
TE1
C1
CA
LLA
LL0.
13IN
TER
NA
L - Z
ON
AL
(GV
): R
ight
Win
g Fi
xed
Lead
ing
Edg
e C
ompa
rtmen
tZo
nal I
nspe
ctio
n: In
tern
al -
Rig
ht W
ing
Fixe
d Le
adin
g E
dge
Com
partm
ent (
EZA
P)
AC
CE
SS
NO
TE: A
ll lo
wer
pan
els
rem
oved
U58
57-6
00-0
405
-21-
01-2
1014
NO
TE8
C8
CA
LLA
LL0.
34IN
TER
NA
L - Z
ON
AL
(GV
): R
ight
Win
g In
ters
par B
ox S
ectio
nZo
nal I
nspe
ctio
n: In
tern
al -
Rig
ht W
ing
Inte
rspa
r Box
Sec
tion
(EZA
P)
AC
CE
SS
NO
TE: A
ll pa
nels
rem
oved
U59
57-6
00-0
505
-21-
01-2
1014
NO
TE8
C8
CA
LLA
LL0.
08IN
TER
NA
L - Z
ON
AL
(GV
): R
ight
Win
g V
ent B
oxZo
nal I
nspe
ctio
n: In
tern
al -
Rig
ht W
ing
Ven
t Box
(EZA
P)
AC
CE
SS
NO
TE: A
ll pa
nels
rem
oved
U60
57-6
00-0
605
-21-
01-2
1012
1207
A12
08C
1238
A12
40A
1251
A12
52A
4 C
4 C
ALL
ALL
0.07
INTE
RN
AL
- ZO
NA
L (G
V):
Rig
ht W
ing
Tip
Ass
embl
yZo
nal I
nspe
ctio
n: In
tern
al -
Rig
ht W
ing
Tip
Ass
embl
y, S
TA X
w
560
U61
57-6
00-0
705
-21-
01-2
1016
NO
TE1
C1
CA
LLA
LL0.
07IN
TER
NA
L - Z
ON
AL
(GV
): Fi
xed
Trai
ling
Edg
e C
ompa
rtmen
t, in
clud
ing
Flap
Hin
ge A
rea
Zona
l Ins
pect
ion:
Inte
rnal
- Fi
xed
Trai
ling
Edg
e C
ompa
rtmen
t, in
clud
ing
Flap
Hin
ge A
rea
(EZA
P)
AC
CE
SS
NO
TE: A
ll hi
nged
pan
els
low
ered
62A
TA 7
1: P
OW
ER P
LAN
T
U63
71-4
00-0
105
-21-
01-2
1070 80
1 A
1 A
ALL
ALL
0.20
EXT
ER
NA
L - Z
ON
AL
(GV
): P
ower
plan
ts, P
ylon
s, C
owl D
oors
, In
let A
reas
, and
Nos
e C
owls
Zona
l Ins
pect
ion:
Ext
erna
l - P
ower
plan
ts, P
ylon
s, C
owl D
oors
, In
let A
reas
, and
Nos
e C
owls
from
gro
und
leve
l
U64
71-4
00-0
205
-21-
01-2
1070 80
2 C
2 C
ALL
ALL
0.40
EXT
ER
NA
L - Z
ON
AL
(GV
): P
ower
plan
ts, P
ylon
s, C
owl D
oors
, In
let A
reas
, and
Nos
e C
owls
Zona
l Ins
pect
ion:
Ext
erna
l - P
ower
plan
ts, P
ylon
s, C
owl D
oors
, In
let A
reas
, and
Nos
e C
owls
Rev 0 19 March 2014
4-13
MD-80 MAINTENANCE MANUAL
0 1 2 3 4
ZON
EAC
CES
S
INTE
RVA
L
THR
ES.
REP
EAT
APPL
ICAB
ILIT
Y
APL
ENG
MAN
-N
OITPIR
CSED
KSATS
RU
OH
DC
-9-8
0SF
Mai
nten
ance
Pla
nnin
g D
ocum
ent
ZON
AL
INSP
ECTI
ON
PR
OG
RA
M
MPD
ITEM
NU
MB
ERAM
M
REF
EREN
CE
U65
71-4
00-0
305
-21-
01-2
1073 74
1 C
1 C
ALL
ALL
0.17
INTE
RN
AL
- ZO
NA
L (G
V):
Pow
erpl
ant N
ose
Cow
ls In
let A
rea
Zona
l Ins
pect
ion:
Inte
rnal
- Le
ft&R
ight
Pow
erpl
ant N
ose
Cow
ls
Inle
t Are
a
U66
71-4
00-0
405
-21-
01-2
1073 74
NO
TE2
C2
CA
LLA
LL0.
40IN
TER
NA
L - Z
ON
AL
(GV
): P
ower
plan
t Nos
e C
owls
Zona
l Ins
pect
ion:
Inte
rnal
- Le
ft&R
ight
Pow
erpl
ant N
ose
Cow
ls
(EZA
P)
AC
CE
SS
NO
TE: A
ll P
anel
s R
emov
ed
U67
71-4
00-0
505
-21-
01-2
1071 72 77 78
NO
TE1
A1
AA
LLA
LL0.
42IN
TER
NA
L - Z
ON
AL
(GV
): P
ower
plan
t&N
acel
le D
oors
Zona
l Ins
pect
ion:
Inte
rnal
- Le
ft&R
ight
Pow
erpl
ant&
Nac
elle
D
oors
(EZA
P)
AC
CE
SS
NO
TE: N
acel
le D
oors
Ope
n
U68
71-4
00-0
605
-21-
01-2
1075 76
NO
TE1
C1
CA
LLA
LL0.
17IN
TER
NA
L - Z
ON
AL
(GV
): E
xhau
st C
one&
Noz
zle
Ass
embl
yZo
nal I
nspe
ctio
n: In
tern
al -
Left&
Rig
ht E
xhau
st C
one&
Noz
zle
Ass
embl
y (E
ZAP
)
AC
CE
SS
NO
TE: E
xhau
st
U69
71-4
00-0
705
-21-
01-2
1081 82
NO
TE2
C2
CA
LLA
LL0.
50IN
TER
NA
L - Z
ON
AL
(GV
): P
ylon
sZo
nal I
nspe
ctio
n: In
tern
al -
Left&
Rig
ht P
ylon
s. (E
ZAP
)
AC
CE
SS
NO
TE: A
ll Lo
wer
Pan
els
Rem
oved
Rev 0 19 March 2014
4-14
MD-80 MAINTENANCE MANUAL
Intentionally Left Blank
Rev 0 19 March 2014
5-1
MD-80 MAINTENANCE MANUAL
CHAPTER 5: SOURCE DOCUMENTS FOR TASKS
5.1 Scope
This chapter of the MPD outlines the SOURCE DOCUMENTS FOR TASKS.
TASK SOURCE CARD DOCUMENT
SOURCE DOCU-MENT REFER-
ENCE
DOCUMENT REVI-SION NO.
DOCUMENT DATE MPD ITEM NO.
MPD ME80-020 0 Aug 2008 05-01-01
MPD ME80-020 0 Aug 2008 05-01-02
MRB ME-MRB-80 3 Aug 2008 20-10-01
MRB ME-MRB-80 3 Aug 2008 20-10-02
MRB ME-MRB-80 3 Aug 2008 20-10-03
MRB ME-MRB-80 3 Aug 2008 20-10-04
MRB ME-MRB-80 3 Aug 2008 20-10-05
MRB ME-MRB-80 3 Aug 2008 20-10-06
MID ME80-016 3 25SEP09 20-10-07
MID ME80-016 3 25SEP09 20-10-08
MID ME80-016 3 25SEP09 20-10-09
MID ME80-016 3 25SEP09 20-10-10
MID ME80-016 3 25SEP09 20-10-11
MID ME80-016 3 25SEP09 20-10-12
MID ME80-016 3 25SEP09 20-10-13
MRB ME-MRB-80 6 Feb 2012 20-10-14
MRB ME-MRB-80 3 Aug 2008 20-020-01
MRB ME-MRB-80 3 Aug 2008 20-020-02
MID ME80-016 3 25SEP09 20-020-04
MRB ME-MRB-80 3 Aug 2008 20-030-01
MID ME80-016 3 25SEP09 20-030-02
MID ME80-016 3 25SEP09 20-040-01
MID ME80-016 3 25SEP09 20-050-01
MID ME80-016 3 25SEP09 20-050-02
MID ME80-016 3 25SEP09 20-060-01
MID ME80-016 3 25SEP09 20-060-02
Rev 0 19 March 2014
5-2
MD-80 MAINTENANCE MANUAL
TASK SOURCE CARD DOCUMENT
SOURCE DOCU-MENT REFER-
ENCE
DOCUMENT REVI-SION NO.
DOCUMENT DATE MPD ITEM NO.
SL MD80-SL-21-103 0 04-20-06 21-01-00
MRB ME-MRB-80 3 Aug 2008 21-021-01
MRB ME-MRB-80 3 Aug 2008 21-021-02
MRB ME-MRB-80 3 Aug 2008 21-022-01
MRB ME-MRB-80 3 Aug 2008 21-022-02
MRB ME-MRB-80 3 Aug 2008 21-022-03
MRB ME-MRB- 80 3 Aug 2008 21-022-04
MRB ME-MRB-80 3 Aug 2008 21-026-01
MRB ME-MRB-80 3 Aug 2008 21-029-01
MRB ME-MRB-80 3 Aug 2008 21-031-01
MRB ME-MRB-80 3 Aug 2008 21-031-02
MRB ME-MRB-80 3 Aug 2008 21-031-03
MRB ME-MRB-80 3 Aug 2008 21-031-04
MRB ME-MRB-80 3 Aug 2008 21-031-05
MRB ME-MRB-80 3 Aug 2008 21-031-06
SL MD80-SL-21-102 0 09-22-03 21-032-05
MRB ME-MRB-80 3 Aug 2008 21-033-01
MRB ME-MRB-80 3 Aug 2008 21-034-01
MRB ME-MRB-80 3 Aug 2008 21-034-02
MRB ME-MRB-80 3 Aug 2008 21-034-03
MRB ME-MRB-80 3 Aug 2008 21-034-04
MRB ME-MRB-80 3 Aug 2008 21-034-05
MRB ME-MRB-80 3 Aug 2008 21-053-01
MRB ME-MRB- 80 3 Aug 2008 21-053-02
MRB ME-MRB-80 3 Aug 2008 21-053-03
MRB ME-MRB- 80 3 Aug 2008 21-054-01
Rev 0 19 March 2014
5-3
MD-80 MAINTENANCE MANUAL
TASK SOURCE CARD DOCUMENT
SOURCE DOCU-MENT REFER-
ENCE
DOCUMENT REVI-SION NO.
DOCUMENT DATE MPD ITEM NO.
MRB ME-MRB-80 3 Aug 2008 21-055-02
MRB ME-MRB-80 3 Aug 2008 21-055-03
MRB ME-MRB-80 3 Aug 2008 21-056-03
MRB ME-MRB-80 3 Aug 2008 21-056-04
MRB ME-MRB-80 3 Aug 2008 21-056-05
MRB ME-MRB- 80 3 Aug 2008 21-062-01
MRB ME-MRB-80 3 Aug 2008 21-062-02
CMR MDC-J1271 L 01-16-03 22-01-00
MRB ME-MRB-80 3 Aug 2008 22-01-01
MRB ME-MRB-80 3 Aug 2008 22-01-02
MRB ME-MRB-80 3 Aug 2008 22-01-03
CMR MDC-J1271 L 01-16-03 22-02-00
CMR MDC-J1271 N 05-07-04 22-03-00
CMR MDC-J1271 L 01-16-03 22-04-00
MRB ME-MRB-80 3 Aug 2008 23-030-01
MRB ME-MRB-80 3 Aug 2008 23-030-02
MRB ME-MRB-80 3 Aug 2008 23-060-01
MRB ME-MRB- 80 3 Aug 2008 23-071-01
MRB ME-MRB- 80 3 Aug 2008 23-071-02
SCI MDC-92K9145 D 01/18/08 24-01-00
MRB ME-MRB-80 3 Aug 2008 24-01-01
MRB ME-MRB-80 3 Aug 2008 24-01-02
MRB ME-MRB-80 3 Aug 2008 24-01-03
MRB ME-MRB-80 3 Aug 2008 24-01-07
MRB ME-MRB-80 3 Aug 2008 24-01-08
MRB ME-MRB-80 3 Aug 2008 24-01-09
Rev 0 19 March 2014
5-4
MD-80 MAINTENANCE MANUAL
TASK SOURCE CARD DOCUMENT
SOURCE DOCU-MENT REFER-
ENCE
DOCUMENT REVI-SION NO.
DOCUMENT DATE MPD ITEM NO.
MRB ME-MRB-80 3 Aug 2008 24-01-10
MRB ME-MRB-80 3 Aug 2008 24-01-11
MRB ME-MRB-80 5 Feb 2009 24-01-12
MRB ME-MRB-80 5 Feb 2009 24-01-13
AOL 9-2160 1 Sep 1991 24-921-60
MRB ME-MRB-80 3 Aug 2008 25-015-01
MRB ME-MRB-80 3 Aug 2008 25-015-02
MRB ME-MRB-80 3 Aug 2008 25-015-03
MRB ME-MRB-80 3 Aug 2008 25-015-04
MRB ME-MRB-80 3 Aug 2008 25-015-05
MRB ME-MRB-80 7 Feb 2013 25-015-06
MRB ME-MRB-80 3 Aug 2008 25-023-01
MRB ME-MRB-80 3 Aug 2008 25-023-02
MRB ME-MRB-80 3 Aug 2008 25-023-04
MRB ME-MRB-80 7 Feb 2013 25-023-05
MRB ME-MRB-80 3 Aug 2008 25-023-06
MRB ME-MRB-80 3 Aug 2008 25-023-07
MRB ME-MRB-80 3 Aug 2008 25-023-08
MRB ME-MRB-80 5 Feb 2011 25-050-01
MRB ME-MRB-80 3 Aug 2008 25-060-03
MRB ME-MRB-80 7 Feb 2013 25-060-05
MRB ME-MRB-80 7 Feb 2013 25-060-06
MRB ME-MRB-80 3 Aug 2008 25-060-07
MRB ME-MRB-80 7 Aug 2008 25-060-09
MRB ME-MRB-80 3 Aug 2008 25-060-10
MRB ME-MRB-80 3 Aug 2008 25-060-11
Rev 0 19 March 2014
5-5
MD-80 MAINTENANCE MANUAL
TASK SOURCE CARD DOCUMENT
SOURCE DOCU-MENT REFER-
ENCE
DOCUMENT REVI-SION NO.
DOCUMENT DATE MPD ITEM NO.
MRB ME-MRB-80 3 Aug 2008 25-060-20
MRB ME-MRB-80 3 Aug 2008 25-060-21
MRB ME-MRB-80 7 Feb 2013 25-060-22
MRB ME-MRB-80 7 Feb 2013 25-060-25
MRB ME-MRB-80 7 Aug 2008 25-060-26
MRB ME-MRB-80 3 Aug 2008 26-12-01
MRB ME-MRB-80 3 Aug 2008 26-12-02
MRB ME-MRB-80 3 Aug 2008 26-021-01
MRB ME-MRB-80 3 Aug 2008 26-021-03
MRB ME-MRB-80 3 Aug 2008 26-021-04
MRB ME-MRB-80 5 Feb 2011 26-021-05
MRB ME-MRB-80 3 Aug 2008 26-021-06
SL MD-80-SL-26-107 0 15Nov11 26-021-08
MRB ME-MRB-80 3 Aug 2008 26-023-01
MRB ME-MRB-80 3 Aug 2008 26-023-02
MRB ME-MRB-80 3 Aug 2008 26-023-03
MRB ME-MRB-80 3 Aug 2008 26-023-07
SL MD80-SL-27-104 0 10-28-04 27-01-00
AD 2001-24-27 0 01-16-02 27-02-00
CMR MDC-J1271 L 01-16-03 27-03-00
MRB ME-MRB-80 3 Aug 2008 27-11-01
MRB ME-MRB-80 3 Aug 2008 27-11-02
MRB ME-MRB-80 3 Aug 2008 27-11-03
MRB ME-MRB- 80 3 Aug 2008 27-11-04
MRB ME-MRB-80 3 Aug 2008 27-11-05
MRB ME-MRB-80 3 Aug 2008 27-11-06
Rev 0 19 March 2014
5-6
MD-80 MAINTENANCE MANUAL
TASK SOURCE CARD DOCUMENT
SOURCE DOCU-MENT REFER-
ENCE
DOCUMENT REVI-SION NO.
DOCUMENT DATE MPD ITEM NO.
MRB ME-MRB-80 3 Aug 2008 27-12-01
MRB ME-MRB-80 3 Aug 2008 27-12-02
MRB ME-MRB-80 3 Aug 2008 27-12-03
MRB ME-MRB-80 3 Aug 2008 27-021-01
MRB ME-MRB-80 3 Aug 2008 27-021-02
MRB ME-MRB-80 3 Aug 2008 27-023-01
MRB ME-MRB-80 3 Aug 2008 27-031-01
MRB ME-MRB-80 3 Aug 2008 27-031-02
MRB ME-MRB-80 3 Aug 2008 27-033-01
MRB ME-MRB-80 3 Aug 2008 27-041-02
MRB ME-MRB-80 3 Aug 2008 27-041-03
SCI MDC-92K145 H 1/18/08 27-041-04
MRB ME-MRB-80 3 Aug 2008 27-042-01
MRB ME-MRB-80 3 Aug 2008 27-051-01
MRB ME-MRB-80 3 Aug 2008 27-051-02
MRB ME-MRB- 80 3 Aug 2008 27-051-03
MRB ME-MRB-80 3 Aug 2008 27-055-01
MRB ME-MRB-80 3 Aug 2008 27-061-01
MRB ME-MRB-80 3 Aug 2008 27-061-02
MRB ME-MRB-80 3 Aug 2008 27-062-01
MRB ME-MRB-80 3 Aug 2008 27-063-01
MRB ME-MRB-80 3 Aug 2008 27-063-02
MRB ME-MRB-80 3 Aug 2008 27-063-03
MRB ME-MRB-80 3 Aug 2008 27-063-04
MRB ME-MRB-80 3 Aug 2008 27-067-01
MRB ME-MRB-80 3 Aug 2008 27-081-01
Rev 0 19 March 2014
5-7
MD-80 MAINTENANCE MANUAL
TASK SOURCE CARD DOCUMENT
SOURCE DOCU-MENT REFER-
ENCE
DOCUMENT REVI-SION NO.
DOCUMENT DATE MPD ITEM NO.
MRB ME-MRB-80 3 Aug 2008 27-081-02
MRB ME-MRB-80 3 Aug 2008 27-081-03
MRB ME-MRB-80 3 Aug 2008 27-081-04
MRB ME-MRB-80 3 Aug 2008 27-081-05
MRB ME-MRB-80 3 Aug 2008 28-11-01
MRB ME-MRB-80 3 Aug 2008 28-12-01
MRB ME-MRB-80 3 Aug 2008 28-12-03
MRB ME-MRB-80 3 Aug 2008 28-12-05
MRB ME-MRB- 80 3 Aug 2008 28-013-01
MRB ME-MRB-80 3 Aug 2008 28-013-02
MRB ME-MRB-80 3 Aug 2008 28-013-03
MRB ME-MRB-80 3 Aug 2008 28-013-04
MRB ME-MRB-80 3 Aug 2008 28-022-02
MRB ME-MRB-80 3 Aug 2008 28-022-03
MRB ME-MRB-80 3 Aug 2008 28-022-04
MRB ME-MRB-80 3 Aug 2008 28-024-01
MRB ME-MRB-80 3 Aug 2008 28-024-03
SCI MDC-92K9145 G 06-07-07 29-01-00
MRB ME-MRB-80 3 Aug 2008 29-12-01
MRB ME-MRB- 80 3 Aug 2008 29-12-02
MRB ME-MRB-80 3 Aug 2008 29-12-03
MRB ME-MRB-80 3 Aug 2008 29-021-01
MRB ME-MRB-80 3 Aug 2008 29-022-01
MRB ME-MRB-80 7 Feb 2013 29-022-02
MRB ME-MRB-80 3 Aug 2008 29-032-01
SB MD80-30-071 2 02-06-96 30-01-00
Rev 0 19 March 2014
5-8
MD-80 MAINTENANCE MANUAL
TASK SOURCE CARD DOCUMENT
SOURCE DOCU-MENT REFER-
ENCE
DOCUMENT REVI-SION NO.
DOCUMENT DATE MPD ITEM NO.
MRB ME-MRB-80 3 Aug 2008 30-10-01
MRB ME-MRB-80 3 Aug 2008 30-10-02
MRB ME-MRB-80 3 Aug 2008 30-10-03
MRB ME-MRB-80 3 Aug 2008 30-10-04
MRB ME-MRB-80 3 Aug 2008 30-10-05
MRB ME-MRB-80 3 Aug 2008 30-10-06
MRB ME-MRB-80 3 Aug 2008 30-10-07
MRB ME-MRB-80 3 Aug 2008 30-10-08
MRB ME-MRB-80 3 Aug 2008 30-030-01
MRB ME-MRB-80 3 Aug 2008 31-031-01
MRB ME-MRB-80 3 Aug 2008 31-031-02
MRB ME-MRB-80 3 Aug 2008 31-051-01
MRB ME-MRB- 80 3 Aug 2008 31-051-02
MRB ME-MRB-80 3 Aug 2008 31-051-03
MRB ME-MRB-80 3 Aug 2008 31-051-04
MRB ME-MRB-80 5 Feb 2011 32-11-01
MRB ME-MRB-80 3 Aug 2008 32-11-03
MRB ME-MRB-80 3 Aug 2008 32-11-04
MRB ME-MRB-80 4 Feb 2009 32-11-05
MRB ME-MRB-80 5 Feb 2011 32-013-02
MRB ME-MRB-80 3 Aug 2008 32-013-05
MRB ME-MRB-80 3 Aug 2008 32-021-03
MRB ME-MRB-80 3 Aug 2008 32-021-04
MRB ME-MRB-80 4 Feb 2009 32-021-05
MRB ME-MRB-80 5 Feb 2011 32-022-02
MRB ME-MRB-80 3 Aug 2008 32-024-02
Rev 0 19 March 2014
5-9
MD-80 MAINTENANCE MANUAL
TASK SOURCE CARD DOCUMENT
SOURCE DOCU-MENT REFER-
ENCE
DOCUMENT REVI-SION NO.
DOCUMENT DATE MPD ITEM NO.
MRB ME-MRB-80 3 Aug 2008 32-031-01
MRB ME-MRB-80 3 Aug 2008 32-031-02
MRB ME-MRB-80 3 Aug 2008 32-031-03
MRB ME-MRB-80 3 Aug 2008 32-031-04
MRB ME-MRB-80 3 Aug 2008 32-031-05
MRB ME-MRB-80 3 Aug 2008 32-031-06
MRB ME-MRB-80 3 Aug 2008 32-031-07
MRB ME-MRB-80 5 Feb 2011 32-035-01
MRB ME-MRB-80 3 Aug 2008 32-035-03
MRB ME-MRB-80 5 Feb 2011 32-041-01
MRB ME-MRB-80 3 Aug 2008 32-041-02
MRB ME-MRB-80 5 Feb 2011 32-042-01
MRB ME-MRB-80 3 Aug 2008 32-043-01
MRB ME-MRB-80 3 Aug 2008 32-044-01
MRB ME-MRB-80 3 Aug 2008 32-044-02
MRB ME-MRB-80 3 Aug 2008 32-044-03
MRB ME-MRB-80 3 Aug 2008 32-044-04
MRB ME-MRB-80 3 Aug 2008 32-044-05
MRB ME-MRB-80 3 Aug 2008 32-044-06
MRB ME-MRB-80 3 Aug 2008 32-044-07
MRB ME-MRB-80 3 Aug 2008 32-044-09
MRB ME-MRB-80 3 Aug 2008 32-045-01
MRB ME-MRB-80 3 Aug 2008 32-045-02
MRB ME-MRB-80 3 Aug 2008 32-051-02
SL MD-80-SL-32-107 0 23JUN03 32-070-01
SL MD-80-SL-32-107 0 23JUN03 32-070-02
Rev 0 19 March 2014
5-10
MD-80 MAINTENANCE MANUAL
TASK SOURCE CARD DOCUMENT
SOURCE DOCU-MENT REFER-
ENCE
DOCUMENT REVI-SION NO.
DOCUMENT DATE MPD ITEM NO.
MRB ME-MRB-80 3 Aug 2008 32-700-01
CMR MDC-J1271 L 01-16-03 33-001-00
SL TIL No 372 B 05-11-01 33-002-00
MRB ME-MRB-80 3 Aug 2008 33-014-01
MRB ME-MRB-80 3 Aug 2008 33-014-02
MRB ME-MRB-80 3 Aug 2008 33-032-01
SL MD80-SL-33-101 0 01-16-03 33-041-03
MRB ME-MRB-80 3 Aug 2008 33-042-01
MRB ME-MRB-80 3 Aug 2008 33-042-02
MRB ME-MRB-80 3 Aug 2008 33-042-03
MRB ME-MRB-80 3 Aug 2008 33-042-04
MRB ME-MRB-80 3 Aug 2008 33-051-01
MRB ME-MRB-80 3 Aug 2008 33-051-02
MRB ME-MRB-80 3 Aug 2008 34-10-01
MRB ME-MRB-80 3 Aug 2008 34-10-02
MRB ME-MRB-80 3 Aug 2008 34-10-03
MRB ME-MRB-80 3 Aug 2008 34-10-04
MRB ME-MRB-80 3 Aug 2008 34-10-05
MRB ME-MRB-80 3 Aug 2008 34-10-06
MRB ME-MRB-80 3 Aug 2008 34-10-07
MRB ME-MRB-80 3 Aug 2008 34-022-01
MRB ME-MRB-80 3 Aug 2008 34-023-01
MRB ME-MRB-80 3 Aug 2008 34-029-01
MRB ME-MRB-80 3 Aug 2008 34-029-02
MRB ME-MRB-80 3 Aug 2008 34-029-03
MRB ME-MRB-80 3 Aug 2008 34-032-02
Rev 0 19 March 2014
5-11
MD-80 MAINTENANCE MANUAL
TASK SOURCE CARD DOCUMENT
SOURCE DOCU-MENT REFER-
ENCE
DOCUMENT REVI-SION NO.
DOCUMENT DATE MPD ITEM NO.
MRB ME-MRB-80 3 Aug 2008 34-046-01
MRB ME-MRB-80 6 Feb 2012 34-054-01
MRB ME-MRB-80 3 Aug 2008 35-10-02
MRB ME-MRB-80 3 Aug 2008 35-10-03
MRB ME-MRB-80 3 Aug 2008 35-10-04
MRB ME-MRB-80 3 Aug 2008 35-10-08
MRB ME-MRB-80 3 Aug 2008 35-10-10
MRB ME-MRB-80 3 Aug 2008 35-10-11
MRB ME-MRB-80 3 Aug 2008 35-030-01
MRB ME-MRB-80 3 Aug 2008 35-030-03
MRB ME-MRB-80 3 Aug 2008 35-030-04
MRB ME-MRB-80 3 Aug 2008 36-015-01
MRB ME-MRB-80 3 Aug 2008 36-015-02
MRB ME-MRB-80 3 Aug 2008 36-024-01
MRB ME-MRB- 80 3 Aug 2008 49-10-01
MRB ME-MRB-80 3 Aug 2008 49-030-02
MRB ME-MRB-80 3 Aug 2008 49-030-03
MRB ME-MRB-80 3 Aug 2008 49-040-01
MRB ME-MRB-80 3 Aug 2008 49-080-01
MRB ME-MRB-80 3 Aug 2008 49-090-01
SL MD-80-SL-53-102A A 11FEB05 51-01-01
SL MD-80-53-106-A A 12/17/08 51-02-01
SL SL MD-80-SL-53-109 0 17Nov11 51-03-01
MRB ME-MRB-80 3 Aug 2008 52-01-02
MRB ME-MRB- 80 3 Aug 2008 52-02-02
MRB ME-MRB-80 3 Aug 2008 52-03-02
Rev 0 19 March 2014
5-12
MD-80 MAINTENANCE MANUAL
TASK SOURCE CARD DOCUMENT
SOURCE DOCU-MENT REFER-
ENCE
DOCUMENT REVI-SION NO.
DOCUMENT DATE MPD ITEM NO.
MRB ME-MRB-80 3 Aug 2008 52-04-02
MRB ME-MRB-80 3 Aug 2008 52-05-02
MRB ME-MRB- 80 3 Aug 2008 52-06-02
MRB ME-MRB- 80 3 Aug 2008 52-07-02
MRB ME-MRB-80 3 Aug 2008 52-08-02
MRB ME-MRB-80 3 Aug 2008 52-09-02
MRB ME-MRB-80 3 Aug 2008 52-10-02
MRB ME-MRB-80 3 Aug 2008 52-11-01
MRB ME-MRB-80 3 Aug 2008 52-11-02
MRB ME-MRB-80 3 Aug 2008 52-11-03
MRB ME-MRB-80 3 Aug 2008 52-11-04
MRB ME-MRB-80 3 Aug 2008 52-12-01
MRB ME-MRB-80 3 Aug 2008 52-12-02
MRB ME-MRB-80 3 Aug 2008 52-12-03
MRB ME-MRB-80 3 Aug 2008 52-021-01
MRB ME-MRB-80 3 Aug 2008 52-021-02
MRB ME-MRB-80 3 Aug 2008 52-021-03
MRB ME-MRB-80 3 Aug 2008 52-021-04
MRB ME-MRB-80 3 Aug 2008 52-030-01
MRB ME-MRB-80 3 Aug 2008 52-030-02
MRB ME-MRB-80 3 Aug 2008 52-030-03
MRB ME-MRB-80 3 Aug 2008 52-030-04
MRB ME-MRB-80 3 Aug 2008 52-041-01
MRB ME-MRB-80 3 Aug 2008 52-041-02
MRB ME-MRB-80 3 Aug 2008 52-041-03
MRB ME-MRB-80 3 Aug 2008 52-042-01
Rev 0 19 March 2014
5-13
MD-80 MAINTENANCE MANUAL
TASK SOURCE CARD DOCUMENT
SOURCE DOCU-MENT REFER-
ENCE
DOCUMENT REVI-SION NO.
DOCUMENT DATE MPD ITEM NO.
MRB ME-MRB-80 3 Aug 2008 52-042-02
MRB ME-MRB-80 3 Aug 2008 52-042-03
MRB ME-MRB-80 3 Aug 2008 52-042-04
MRB ME-MRB-80 3 Aug 2008 52-043-01
MRB ME-MRB-80 3 Aug 2008 52-043-02
MRB ME-MRB-80 3 Aug 2008 52-043-03
MRB ME-MRB-80 3 Aug 2008 52-043-04
MRB ME-MRB-80 3 Aug 2008 52-045-01
MRB ME-MRB-80 3 Aug 2008 52-045-02
MRB ME-MRB-80 3 Aug 2008 52-054-01
MRB ME-MRB-80 3 Aug 2008 52-061-01
MRB ME-MRB-80 3 Aug 2008 52-061-02
MRB ME-MRB-80 3 Aug 2008 52-061-04
MRB ME-MRB-80 3 Aug 2008 52-062-01
MRB ME-MRB-80 3 Aug 2008 52-062-02
MRB ME-MRB-80 3 Aug 2008 52-062-03
MRB ME-MRB-80 3 Aug 2008 52-070-01
MRB ME-MRB-80 3 Aug 2008 52-111-02
MRB ME-MRB- 80 3 Aug 2008 52-112-02
MRB ME-MRB-80 3 Aug 2008 52-800-01
MRB ME-MRB-80 3 Aug 2008 52-800-02
MRB ME-MRB-80 3 Aug 2008 52-800-03
SB DC9-53A295 4 10-20-05 53-003-00
MRB ME-MRB-80 3 Aug 2008 53-013-02
MRB ME-MRB-80 3 Aug 2008 53-014-02
MRB ME-MRB-80 3 Aug 2008 53-015-02
Rev 0 19 March 2014
5-14
MD-80 MAINTENANCE MANUAL
TASK SOURCE CARD DOCUMENT
SOURCE DOCU-MENT REFER-
ENCE
DOCUMENT REVI-SION NO.
DOCUMENT DATE MPD ITEM NO.
MRB ME-MRB-80 3 Aug 2008 53-016-02
MRB ME-MRB-80 3 Aug 2008 53-016-04
MRB ME-MRB-80 3 Aug 2008 53-017-02
MRB ME-MRB-80 3 Aug 2008 53-018-02
MRB ME-MRB-80 3 Aug 2008 53-019-02
MRB ME-MRB-80 3 Aug 2008 53-020-02
MRB ME-MRB-80 3 Aug 2008 53-021-03
MRB ME-MRB-80 3 Aug 2008 53-022-02
MRB ME-MRB- 80 3 Aug 2008 53-023-02
MRB ME-MRB- 80 3 Aug 2008 53-024-02
MRB ME-MRB-80 3 Aug 2008 53-025-02
MRB ME-MRB-80 3 Aug 2008 53-026-02
MRB ME-MRB-80 3 Aug 2008 53-027-02
MRB ME-MRB-80 3 Aug 2008 53-028-02
MRB ME-MRB-80 3 Aug 2008 53-029-02
MRB ME-MRB- 80 3 Aug 2008 53-030-02
MRB ME-MRB-80 3 Aug 2008 53-031-02
MRB ME-MRB-80 3 Aug 2008 53-032-02
MRB ME-MRB-80 3 Aug 2008 53-033-02
MRB ME-MRB-80 3 Aug 2008 53-034-02
MRB ME-MRB-80 3 Aug 2008 53-035-02
MRB ME-MRB-80 3 Aug 2008 53-036-02
MRB ME-MRB-80 3 Aug 2008 53-037-01
MRB ME-MRB-80 3 Aug 2008 53-038-02
MRB ME-MRB- 80 3 Aug 2008 53-038-03
MRB ME-MRB-80 3 Aug 2008 53-038-04
Rev 0 19 March 2014
5-15
MD-80 MAINTENANCE MANUAL
TASK SOURCE CARD DOCUMENT
SOURCE DOCU-MENT REFER-
ENCE
DOCUMENT REVI-SION NO.
DOCUMENT DATE MPD ITEM NO.
MRB ME-MRB-80 3 Aug 2008 53-038-05
MRB ME-MRB-80 3 Aug 2008 53-038-06
MRB ME-MRB-80 3 Aug 2008 53-039-02
MRB ME-MRB-80 3 Aug 2008 53-040-02
MRB ME-MRB-80 3 Aug 2008 53-041-02
MRB ME-MRB-80 3 Aug 2008 53-042-02
MRB ME-MRB-80 3 Aug 2008 53-100-01
MRB ME-MRB-80 3 Aug 2008 53-100-02
MRB ME-MRB-80 3 Aug 2008 53-100-03
MRB ME-MRB-80 3 Aug 2008 53-100-04
MRB ME-MRB-80 3 Aug 2008 53-100-05
MRB ME-MRB-80 3 Aug 2008 53-100-06
MRB ME-MRB-80 3 Aug 2008 53-100-07
MRB ME-MRB-80 3 Aug 2008 53-100-08
MRB ME-MRB-80 3 Aug 2008 53-100-09
MRB ME-MRB-80 3 Aug 2008 53-100-10
MRB ME-MRB-80 3 Aug 2008 53-100-11
MRB ME-MRB-80 3 Aug 2008 53-100-12
MRB ME-MRB-80 3 Aug 2008 53-100-13
MRB ME-MRB-80 3 Aug 2008 53-100-14
MRB ME-MRB-80 3 Aug 2008 53-100-15
MRB ME-MRB-80 3 Aug 2008 53-100-16
MRB ME-MRB-80 3 Aug 2008 53-100-17
MID ME80-016 3 25SEP09 53-100-18
MID ME80-016 3 25SEP09 53-100-19
MRB ME-MRB-80 3 Aug 2008 53-103-02
Rev 0 19 March 2014
5-16
MD-80 MAINTENANCE MANUAL
TASK SOURCE CARD DOCUMENT
SOURCE DOCU-MENT REFER-
ENCE
DOCUMENT REVI-SION NO.
DOCUMENT DATE MPD ITEM NO.
MRB ME-MRB- 80 3 Aug 2008 53-139-02
MRB ME-MRB-80 3 Aug 2008 53-139-03
MRB ME-MRB-80 3 Aug 2008 53-139-04
MRB ME-MRB-80 3 Aug 2008 53-139-05
MRB ME-MRB-80 3 Aug 2008 53-140-02
MRB ME-MRB-80 3 Aug 2008 53-140-03
MRB ME-MRB-80 3 Aug 2008 53-200-01
MRB ME-MRB-80 3 Aug 2008 53-200-02
MRB ME-MRB-80 3 Aug 2008 53-200-03
MRB ME-MRB-80 3 Aug 2008 53-200-04
MRB ME-MRB-80 3 Aug 2008 53-200-05
MRB ME-MRB- 80 3 Aug 2008 53-200-06
MRB ME-MRB- 80 3 Aug 2008 53-300-01
MRB ME-MRB- 80 3 Aug 2008 53-300-02
MRB ME-MRB-80 3 Aug 2008 53-300-03
MRB ME-MRB-80 3 Aug 2008 53-300-04
MRB ME-MRB-80 3 Aug 2008 54-044-02
MRB ME-MRB-80 3 Aug 2008 54-045-02
MRB ME-MRB-80 3 Aug 2008 54-046-02
MRB ME-MRB-80 3 Aug 2008 54-047-02
MRB ME-MRB-80 3 Aug 2008 54-048-02
MRB ME-MRB-80 3 Aug 2008 54-049-02
MRB ME-MRB-80 3 Aug 2008 55-050-01
MRB ME-MRB-80 3 Aug 2008 55-050-02
MRB ME-MRB-80 3 Aug 2008 55-051-01
MRB ME-MRB-80 3 Aug 2008 55-051-02
Rev 0 19 March 2014
5-17
MD-80 MAINTENANCE MANUAL
TASK SOURCE CARD DOCUMENT
SOURCE DOCU-MENT REFER-
ENCE
DOCUMENT REVI-SION NO.
DOCUMENT DATE MPD ITEM NO.
MRB ME-MRB-80 3 Aug 2008 55-052-02
MRB ME-MRB-80 3 Aug 2008 55-053-02
MRB ME-MRB-80 3 Aug 2008 55-054-02
MRB ME-MRB-80 3 Aug 2008 55-055-02
MRB ME-MRB-80 3 Aug 2008 55-056-02
MRB ME-MRB-80 3 Aug 2008 55-057-02
MRB ME-MRB-80 3 Aug 2008 55-058-02
MRB ME-MRB-80 3 Aug 2008 55-059-02
MRB ME-MRB-80 3 Aug 2008 55-059-03
MRB ME-MRB-80 3 Aug 2008 55-060-02
MRB ME-MRB-80 3 Aug 2008 55-061-02
MRB ME-MRB-80 3 Aug 2008 55-062-02
MRB ME-MRB-80 3 Aug 2008 55-063-01
MRB ME-MRB-80 3 Aug 2008 55-064-01
MRB ME-MRB-80 3 Aug 2008 55-064-03
MRB ME-MRB-80 3 Aug 2008 55-064-04
MRB ME-MRB-80 3 Aug 2008 55-065-02
MRB ME-MRB-80 3 Aug 2008 55-066-02
MRB ME-MRB-80 3 Aug 2008 55-067-02
MRB ME-MRB-80 3 Aug 2008 55-163-01
MRB ME-MRB-80 3 Aug 2008 55-163-02
MRB ME-MRB-80 3 Aug 2008 55-300-05
MRB ME-MRB-80 3 Aug 2008 55-300-06
MRB ME-MRB-80 7 Feb 2012 55-300-07
MID ME80-016 3 25SEP09 55-300-08
MRB ME-MRB-80 6 Feb 2012 56-11-01
Rev 0 19 March 2014
5-18
MD-80 MAINTENANCE MANUAL
TASK SOURCE CARD DOCUMENT
SOURCE DOCU-MENT REFER-
ENCE
DOCUMENT REVI-SION NO.
DOCUMENT DATE MPD ITEM NO.
MRB ME-MRB-80 3 Aug 2008 56-12-01
MRB ME-MRB-80 3 Aug 2008 56-12-02
MRB ME-MRB-80 3 Aug 2008 56-12-03
MRB ME-MRB-80 3 Aug 2008 56-021-01
SL MD-80-SL-57-116 0 01-15-09 57-002-00
SL MD-80-SL-57-116 0 01-15-09 57-003-00
MRB ME-MRB-80 3 Aug 2008 57-068-02
MRB ME-MRB-80 3 Aug 2008 57-069-02
MRB ME-MRB-80 3 Aug 2008 57-070-01
MRB ME-MRB-80 3 Aug 2008 57-070-02
MRB ME-MRB-80 3 Aug 2008 57-071-02
MRB ME-MRB-80 3 Aug 2008 57-072-02
MRB ME-MRB-80 3 Aug 2008 57-072-03
MRB ME-MRB-80 3 Aug 2008 57-073-02
MRB ME-MRB-80 3 Aug 2008 57-074-02
MRB ME-MRB-80 3 Aug 2008 57-074-03
MRB ME-MRB-80 3 Aug 2008 57-075-02
MRB ME-MRB-80 3 Aug 2008 57-075-03
MRB ME-MRB-80 3 Aug 2008 57-076-02
MRB ME-MRB-80 3 Aug 2008 57-076-03
MRB ME-MRB-80 3 Aug 2008 57-077-02
MRB ME-MRB-80 3 Aug 2008 57-078-02
MRB ME-MRB-80 3 Aug 2008 57-079-02
MRB ME-MRB-80 3 Aug 2008 57-079-03
MRB ME-MRB-80 3 Aug 2008 57-080-02
MRB ME-MRB-80 3 Aug 2008 57-080-03
Rev 0 19 March 2014
5-19
MD-80 MAINTENANCE MANUAL
TASK SOURCE CARD DOCUMENT
SOURCE DOCU-MENT REFER-
ENCE
DOCUMENT REVI-SION NO.
DOCUMENT DATE MPD ITEM NO.
MRB ME-MRB-80 3 Aug 2008 57-081-02
MRB ME-MRB-80 3 Aug 2008 57-082-02
MRB ME-MRB-80 3 Aug 2008 57-082-03
MRB ME-MRB-80 3 Aug 2008 57-083-02
MRB ME-MRB-80 3 Aug 2008 57-084-02
MRB ME-MRB-80 3 Aug 2008 57-085-02
MRB ME-MRB-80 3 Aug 2008 57-086-02
MRB ME-MRB-80 3 Aug 2008 57-087-02
MRB ME-MRB-80 3 Aug 2008 57-088-02
MRB ME-MRB-80 3 Aug 2008 57-089-02
MRB ME-MRB-80 3 Aug 2008 57-090-02
MRB ME-MRB-80 3 Aug 2008 57-091-01
MRB ME-MRB-80 3 Aug 2008 57-091-02
MRB ME-MRB-80 3 Aug 2008 57-092-01
MRB ME-MRB-80 3 Aug 2008 57-092-03
MRB ME-MRB-80 3 Aug 2008 57-093-01
MRB ME-MRB-80 3 Aug 2008 57-093-03
MRB ME-MRB-80 3 Aug 2008 57-094-03
MRB ME-MRB-80 3 Aug 2008 57-095-02
MRB ME-MRB-80 3 Aug 2008 57-096-02
MRB ME-MRB-80 3 Aug 2008 57-500-01
MRB ME-MRB-80 3 Aug 2008 57-500-02
MRB ME-MRB-80 3 Aug 2008 57-500-03
MRB ME-MRB-80 3 Aug 2008 57-500-04
MRB ME-MRB-80 3 Aug 2008 57-500-05
MRB ME-MRB-80 3 Aug 2008 57-500-06
Rev 0 19 March 2014
5-20
MD-80 MAINTENANCE MANUAL
TASK SOURCE CARD DOCUMENT
SOURCE DOCU-MENT REFER-
ENCE
DOCUMENT REVI-SION NO.
DOCUMENT DATE MPD ITEM NO.
MRB ME-MRB-80 3 Aug 2008 57-500-07
MRB ME-MRB-80 3 Aug 2008 57-600-01
MRB ME-MRB-80 3 Aug 2008 57-600-02
MRB ME-MRB-80 3 Aug 2008 57-600-03
MRB ME-MRB-80 3 Aug 2008 57-600-04
MRB ME-MRB-80 3 Aug 2008 57-600-05
MRB ME-MRB-80 3 Aug 2008 57-600-06
MRB ME-MRB-80 3 Aug 2008 57-600-07
MRB ME-MRB-80 3 Aug 2008 71-10-01
MRB ME-MRB-80 3 Aug 2008 71-10-05
MRB ME-MRB-80 3 Aug 2008 71-10-06
MRB ME-MRB-80 3 Aug 2008 71-10-10
MRB ME-MRB-80 3 Aug 2008 71-10-11
MRB ME-MRB-80 3 Aug 2008 71-10-12
MRB ME-MRB-80 3 Aug 2008 71-10-13
MRB ME-MRB-80 3 Aug 2008 71-10-14
AOL AOL 9-2624 0 10-09-01 71-10-15
MRB ME-MRB-80 7 Feb 2013 71-10-16
MRB ME-MRB-80 3 Aug 2008 71-020-01
MRB ME-MRB-80 3 Aug 2008 71-020-02
MRB ME-MRB- 80 3 Aug 2008 71-020-04
MRB ME-MRB-80 5 Feb 2011 71-030-01
MRB ME-MRB-80 3 Aug 2008 71-071-02
MRB ME-MRB-80 3 Aug 2008 71-400-01
MRB ME-MRB-80 3 Aug 2008 71-400-02
MRB ME-MRB-80 3 Aug 2008 71-400-03
Rev 0 19 March 2014
5-21
MD-80 MAINTENANCE MANUAL
TASK SOURCE CARD DOCUMENT
SOURCE DOCU-MENT REFER-
ENCE
DOCUMENT REVI-SION NO.
DOCUMENT DATE MPD ITEM NO.
MRB ME-MRB-80 3 Aug 2008 71-400-04
MRB ME-MRB-80 3 Aug 2008 71-400-05
MRB ME-MRB-80 3 Aug 2008 71-400-06
MRB ME-MRB-80 3 Aug 2008 71-400-07
MRB ME-MRB-80 3 Aug 2008 72-020-01
MRB ME-MRB-80 3 Aug 2008 72-030-01
MRB ME-MRB-80 3 Aug 2008 72-030-03
MRB ME-MRB-80 3 Aug 2008 72-030-04
MRB ME-MRB-80 3 Aug 2008 72-050-01
MRB ME-MRB-80 3 Aug 2008 72-050-02
MRB ME-MRB-80 3 Aug 2008 72-050-03
MRB ME-MRB-80 3 Aug 2008 72-060-01
MRB ME-MRB-80 3 Aug 2008 73-01-02
MRB ME-MRB-80 3 Aug 2008 74-01-01
MRB ME-MRB-80 3 Aug 2008 76-11-01
AOL AOL 9-2096B B 10-01-91 76-11-02
MRB ME-MRB-80 3 Aug 2008 76-013-01
MRB ME-MRB-80 3 Aug 2008 76-021-01
MRB ME-MRB-80 3 Aug 2008 76-021-02
MRB ME-MRB-80 3 Aug 2008 78-030-02
MRB ME-MRB-80 3 Aug 2008 78-030-03
MRB ME-MRB-80 3 Aug 2008 79-01-02
MRB ME-MRB-80 3 Aug 2008 79-030-01
MRB ME-MRB-80 3 Aug 2008 80-01-01
MRB ME-MRB-80 3 Aug 2008 80-01-02
MPD ME80-020 3 01AUG08 80-01-03
Rev 0 19 March 2014
5-22
MD-80 MAINTENANCE MANUAL
Intentionally Left Blank
Rev 0 19 March 2014
6-1
MD-80 MAINTENANCE MANUAL
CHAPTER 6: WEIGHT AND BALANCE PROCEDURES
6.1 Policies
6.1.1 General
The purpose of this Chapter is to set forth methods, procedures and responsibilities for maintaining weight and balance control of EVERTS AIR CARGO's fleet of aircraft.
A complete weight and balance file shall be maintained for each aircraft. Each weight and balance file shall be kept up to date in the maintenance files of the Company, and shall include the following:
1. A current equipment list as weighed. (Form M-9B)
2. A current copy of the Aircraft Actual Weight and Balance. (Form M-9)
3. A current copy of the Weight and Balance Report. (Form M-9E)
4. An accumulative Weight Change Record. (Form M-9G)
5. A signed copy of form M-9H.
6.1.2 Responsibilities
It shall be the responsibility of the Chief Inspector to establish and maintain the procedures and records outlined in this chapter for the control and periodic weighing and weight and balance changes affecting the Company Aircraft.
It shall be the responsibility of the Director of Operations to establish and maintain procedures which will ensure that the aircraft are properly loaded and will not exceed the authorized gross weight and center of gravity limits.
6.1.3 Controlling Documents
1. The Company's Operations Specifications, Part E, "Aircraft Weight and Balance Control."
2. FAA approved Flight Manual appropriate to the type of aircraft.
3. Weight and Balance Control during flight operations (including loading schedule instructions) are contained in the Company's Operations Manual.
4. Boeing Weight and Balance for S/N 49470.
5. AEI Weight and Balance Manual Supplement R-846 MDCJ8358.
6.2 Weight and Balance Control
6.2.1 Individual Aircraft Weight and Balance Control
The individual weight and balance of each aircraft shall be reestablished at the specified reweighing peri-ods. It shall also be reestablished whenever the cumulative changes to the empty weight exceed plus or minus one half of one percent of the maximum landing weight or the cumulative change in CG position exceeds one half of one percent of the CG range.
6.2.2 Responsibility
The Chief Inspector will be responsible for current empty aircraft weight and balance. Prior to release of an aircraft which has undergone a repair or alteration affecting the weight and balance of the aircraft, the Chief Inspector will accomplish the following as applicable:
Rev 0 19 March 2014
6-2
MD-80 MAINTENANCE MANUAL
If the cumulative weight change is less than plus or minus one half of one percent of the CG range, the cumulative change in weight and balance will be recorded on the Aircraft Basic Weight and Balance Report, Form M-9G.
When the cumulative weight changes to the empty weight exceed plus or minus one half of one percent of the maximum landing weight, recompute the empty weight.
When the cumulative change in the CG position exceeds plus or minus one half of one percent of the CG Range, recompute the empty weight CG.
The recomputed aircraft empty weight and balance shall be forwarded to the Operations Secretary using Form M-9H. Form M-9H must be signed and returned to the Chief Inspector prior to release of the aircraft.
Changes to the aircraft CG, empty weight, or cumulative change to the aircraft weight and balance are the responsibility of the Director of Operations. The effects of these factors upon the current loading schedule are also his responsibility.
6.3 Terms and Definitions
6.3.1 Arm
The horizontal distance in inches from the reference datum line to the center of gravity of the item.
6.3.2 Center of Gravity (CG)
The point about which an aircraft would balance if it were possible to suspend it at that point. It is the mass center of the aircraft, or the theoretical point at which the entire weight of the aircraft is assumed to be con-centrated.
6.3.3 Center of Gravity Limits
The specified forward and aft points beyond which the CG must not be located during flight.
6.3.4 Center of Gravity Range
The distance between the forward and aft CG limits.
6.3.5 Datum (REF. Datum)
An imaginary vertical line from which all measurements of arm are taken. All moment arms and the loca-tion of permissible CG range must be taken with reference to that point.
6.3.6 Equipment Check List
The required equipment list plus equipment included in the aircraft empty weight.
6.3.7 Required Equipment List
The required equipment as prescribed in the applicable airworthiness regulations. (See certification basis, Type Certificate Data Sheet appropriate to the type of aircraft).
6.3.8 Moment
The product of the weight of an item multiplied by its arm. Moments are expressed in pounds-inches, (1 lb-in). Total moment is the weight of the aircraft multiplied by the distance between the datum and CG.
Rev 0 19 March 2014
6-3
MD-80 MAINTENANCE MANUAL
6.3.9 Moment Index (or Index)
A moment divided by a constant such as 100. The moment index is used to simplify weight and balance computations where heavy items and long arms result in large, unmanageable numbers.
6.3.10 Station
A location in the aircraft which is identified by a number designating its distance in inches from the datum. The datum is identified as station zero. The station and arm are identical. An item located at station +50 would have an arm of 50 inches.
6.3.11 Basic Weight
The weight of the aircraft, engines, and all items of operating equipment that have fixed locations and are permanently installed in the aircraft.
6.3.12 Empty Weight
The empty weight of the aircraft as weighed for weight and balance purposes, plus all items listed on the master equipment checklist.
6.3.13 Basic Operating Weight
The weight of the aircraft, engines and all items of operating equipment that have fixed locations and are permanently installed in the aircraft, plus crew and all the equipment required for flight but not including fuel and payload.
6.3.14 Basic Operating Index
The particular aircraft index with equipment and crew listed in Item 13.
6.3.15 Operating Index
The index for the particular aircraft, ready to operate with crew, fuel and payload and all required equip-ment.
6.4 Weight and Balance Forms: M-9, M-9A, M-9B, M-9E, M-9G, and M-9H
6.4.1 Pre-Weighing Check List (Form M-9)
This report is used and completed prior to the actual weighing of the aircraft and is attached to the actual Weight and Balance Form for filing. This form shall establish that the aircraft is proper condition to be weighed.
6.4.2 Aircraft Equipment List (Form M-9B)
This form is used to record all permanent equipment installed in the aircraft at the time of weighing. The Chief Inspector is responsible for the accuracy and completeness of this form. It is attached to the actual Weight and Balance Form for retention in the aircraft records.
6.4.3 Aircraft Actual Weight and Balance (Form M-9):
This report is to record and compute the actual weight, CG location, and moment of each aircraft. It is used when the aircraft is weighed and becomes part of the particular Aircraft Weight and Balance file. Data from this report is entered on the Aircraft Basic Weight and Balance Record Form M-9. The Chief Inspec-tor is responsible for the completion of this form and proper distribution. This form will be used for com-
Rev 0 19 March 2014
6-4
MD-80 MAINTENANCE MANUAL
putation of operational index units and percent CG and provides the data required by the flight crews to compute the weight and balance for each flight. M-9E is for an aircraft in Cargo Only configuration.
6.4.4 Accumulative Weight Change Record (Form M-9G)
This form shall be used between aircraft weighing to compute the change in CG caused by any removed or installed equipment, or major repairs which will effect the weight and balance of the aircraft. Weight changes totaled on this sheet may not exceed one-half of 1% of the maximum landing weight or % MAC of the aircraft without recomputing the weight and balance. Any of these sheets accumulated between weighing may be discarded at weighing.
6.4.5 Change to Basic Operating Weight (BOW) (Form M-9H)
This form is issued by the Chief Inspector with the new weight and balance of the aircraft to the Operations Secretary. An Operations Bulletin is then generated and sent to appropriate personnel for posting. This form is returned to the Chief Inspector upon issuance of an Operations Bulletin.
Rev 0 19 March 2014
6-5
MD-80 MAINTENANCE MANUAL
Form M9
AS-WEIGHED DATA, AIRPLANE LEVEL
WEIGHING POINTS (JACKPOINTS)
SCALE READING
TARE SCALE CALIBRATION CORRECTION
NET WEIGHT
(POUNDS)
H-ARM (FUS STA)
MOMENT
LEFT MAIN GEAR
RIGHT MAIN GEAR
SUB-TOTAL (MAIN GEAR) 967.1
NOSE JACK PAD (W ) 98.0
AIRPLANE AS WEIGHED (WT)
BASIC EMPTY WEIGHT FORM M-9E TABLE 1 (BEW)
BASIC OPERATING WEIGHT FORM M-9E TABLE 2 (BOW)
AIRPLANE CG H-ARM (BOW) = _______________ BASIC OPERATIONAL WEIGHT (BOW) = ________________
AIRPLANE CG (%MAC) = ________________ x 100 = _________________ x 100 = _________________ % MAC
INDEX UNIT = 5000 + ______________________ = 5000 + __________________ = ________________ INDEX
STA __________ DATE ____________ A/C N# _____________ A/C TYPE ______________
A/C S/N ______________ DATUM ___________ SCALE MODEL _____________ S/N _____________
SCALE CAL. DATE ____________
COMPUTED BY ____________________________ A+P # ____________________
H-ARM – 885.5
158.5
- 885.5158.5
WEIGHT (H-ARM – 922)1000
( - 922)1000
Rev 0 19 March 2014
6-6
MD-80 MAINTENANCE MANUAL
Form M9
AS-WEIGHED DATA, AIRPLANE LEVEL
WEIGHING POINTS (JACKPOINTS)
SCALE READING
TARE SCALE CALIBRATION CORRECTION
NET WEIGHT
(POUNDS)
H-ARM (FUS STA)
MOMENT
LEFT MAIN GEAR 852.9
RIGHT MAIN GEAR 852.9
SUB-TOTAL (WING JACKS)
AFT FUSELAGE JACK PAD (W ) 1337.3
AIRPLANE AS WEIGHED (WT)
BASIC EMPTY WEIGHT FORM M-9E TABLE 1 (BEW)
BASIC OPERATING WEIGHT FORM M-9E TABLE 2 (BOW)
AIRPLANE CG H-ARM (BOW) = _______________ BASIC OPERATIONAL WEIGHT (BOW) = ________________
AIRPLANE CG (%MAC) = ________________ x 100 = _________________ x 100 = _________________ % MAC
INDEX UNIT = 5000 + ______________________ = 5000 + __________________ = ________________ INDEX
STA __________ DATE ____________ A/C N# _____________ A/C TYPE ______________
A/C S/N ______________ DATUM ___________ SCALE MODEL _____________ S/N _____________
SCALE CAL. DATE ____________
COMPUTED BY ____________________________ A+P # ____________________
H-ARM – 885.5
158.5
- 885.5158.5
WEIGHT (H-ARM – 922)1000
( - 922)1000
Rev 0 19 March 2014
6-7
MD-80 MAINTENANCE MANUAL
6.5 Preweighing Checklist - Form M-9A
Weighing Condition
Cockpit
STA. ______ DATE________________ A/C NO.N _____________ A/C TYPE ________________
A/C SER. NO. ______________ DATUM _______________ INSPECTOR ____________________
Description YES NO N/A MECH INSP
1. Aircraft in hangar with hangar door closed and leveled
2. Install chocks and release parking brake
3. Install gear pins
4. Landing gear strut serviced
5. Tires inflated at normal pressure
6. All flight control neutral, flap and spoiler retracted
7. All fuel tanks and sumps drained
8. Potable water system drained
9. Toilet and lavatory waste water drained
10. All hydraulic systems filled
11. Engine’s oil tanks filled
12. CSD oil systems filled
13. APU oil tank filled
14. Engine and APU fire extinguisher bottles full
15. Clean and set up cockpit and cabin, appropriate for dispatch
Description YES NO N/A MECH INSP
16. Crew oxygen cylinder filled
17. Portable oxygen cylinder in place and filled
18. Hand fire extinguisher in place and filled
19. Oxygen masks in place
20. Life vests installed
21. Hand axe installed
22. First aid kit installed
23. Headphones and microphones installed
24. All radio equipment installed
Rev 0 19 March 2014
6-8
MD-80 MAINTENANCE MANUAL
Lower Cargo Compartments
Cargo Configuration Aircraft
Verify That:
25. All seats and seat belts installed
26. All cockpit instruments installed
27. All cockpit manuals removed
Description YES NO N/A MECH INSP
28. All containers removed
29. Fly away kits removed
30. All compartments empty
Description YES NO N/A MECH INSP
31. Pallet roller system installed
32. Cargo barrier 9G Bulkhead
33. Loading and tie down equipment installed
Description YES NO N/A MECH INSP
34. Accessories, electrical and electronic compart-ments units are installed
35. All tools and working equipment from cabin, cockpit and cargo compartments were removed
36. All aircraft emergency doors closed
37. All aircraft doors and cockpit windows closed
38. Hangar doors closed
39. Nothing interferes with weighing operation in air-craft exterior and interior
40. Airplane equipment in agreement with applicable equipment list (Write down deviation list in sec-tion 6.6 M-9E if not)
41. Aircraft leveled and ready for weighing
42. Weight and balance procedure completed
43. Weigh aircraft and enter weights on M-9
44. After weighing, return aircraft to normal by ser-vicing all systems and reinstalling all removed equipment supplies
Rev 0 19 March 2014
6-9
MD-80 MAINTENANCE MANUAL
6.6 Form M-9E
Table 1: Deviations of Basic Empty Weight (BEW)
Table 2: Calculation of Basic Operating Weight (BOW)
REGISTRATION N _______ A/C TYPE _______ LOCATION _____________ DATE ___________DATE OF LAST WEIGHING _________________ REPORT NUMBER_________________________
Description Weight +/- Arm Inches Moment (in-lbs)
Aircraft as Weighed
Basic Empty Weight (BEW) CG Moment (in-lbs)
Description Weight (+) Arm Inches Moment (in-lbs)
Basic Empty Weight
2 Pilots 390.0 122.0 47580.0
2 Pilots’ Equipment 50.0 118.6 5930.0
1 Aircraft Library 30.0 180.5 5415.0
Cargo Straps (48 ea) 264.0 762.0 201168.0
Fuel Drainable (Unusable) 131.3 911.4 119666.8
Basic Operating Weight CG Moment (in-lbs)
Rev 0 19 March 2014
6-10
MD-80 MAINTENANCE MANUAL
6.7 Accumulative Weight Change Record (Form M-9G)
Aircraft N_____________________ Date_______________ Station______________________________
List all equipment changes (removed or installed) or major repairs which will affect the weight and balance of the aircraft. Weight changes may accumulate not exceeding one half of 1% of the maximum landing weight, or % MAC, without recomputing the weight and balance.
NOTE: See aircraft AFM for maximum landing weight.
Inspector_______________________________________________ Date__________________________
DATE ITEM INSTALLED / REMOVED
WEIGHT +/- ARM MOMENT
Rev 0 19 March 2014
6-11
MD-80 MAINTENANCE MANUAL
6.8 Change to Basic Operating Weight (BOW) Form M-9H
From: EAC Chief Inspector Date_______________
To: EAC Operations Secretary
Subject: Change to Basic Operating Weight
Instructions:
1. Issue an Operations Bulletin to alert operations of the new weight.
2. Complete the bottom section of this form and return to the Chief Inspector.
TO: Chief Inspector Date_______________
FROM: EAC Operations Secretary
Operations Bulletin issued on ________________________________.
1. Aircraft S/N: ___________________ A/C Reg. No. ___________________
2. Date Weighed: ___________________
3. BOW: ___________________
4. Index: ___________________
5. W&B Folders and Log Book Can updated on ___________________________.
6. % MAC _____________________________________
7. C of G ______________________________________
Signature, Chief Inspector
Signature, Operations Secretary
Rev 0 19 March 2014
6-12
MD-80 MAINTENANCE MANUAL
6.9 Aircraft Equipment List
The Weighing Check List is to be used to record the condition of the airplane at time of weighing by indi-cating the “as weighed” status of each item. Applicability to Manufacturer’s Empty Weight (MEW), Stan-dard Basic Empty Weight (SBEW) and Delivery Empty Weight (DEW) conditions are also indicated. Included on the check list here:
1. Items which are loose or readily removable2. Items which have alternates which may be substituted3. Items which are likely to be missing at time of weighing4. Standard Items (defined in Chapter 1)5. Miscellaneous items which may be aboard at time of weighing
The Weighing Check List is also used to adjust the “as weighed” condition of the airplane to an MEW con-dition. Additional “as weighed” and “MEW” weight adjustment columns have been provided for customer use in subsequent weighings and can be used to adjust to SBEW and DEW conditions also. The procedure is as follows:
Compare the “as weighed” status of an item to its MEW applicability. If they are the same (both orboth 0) and MEW adjustment is not required. If they are not the same an MEW adjustment is required and may be accomplished by using one of the following methods:1. If the MEW applicability is indicated by a “ ”, and the “as weighed” status by a “0”, a plus
weight adjustment is required. The amount of the adjustment is determined by multiplying the quantity by the unit weight.
2. If the MEW applicability is indicated by a “0”, and the “as weighed” status by a “ ”, a minus weight adjustment is required, and is determined the same as for method number 1 above.
3. If the “as weighed” quantity is different than the quantity noted on the check list, the “as weighed” quantity should be noted in the “as weighed” column in lieu of a “ ”. Either a plus or minus weight adjustment is required depending on whether the “as weighed” quantity is less or greater than the quantity noted. The amount of the adjustment is determined by multiplying the difference between the “as weighed” quantity and the noted quantity by the unit weight.
The Weighing Check List is not intended to include all equipment items on the airplane. Accordingly, most items with small weight effect have been omitted. If items in this category are missing at time of weighing, they should be added to the check list and an appropriate weight adjustment made.
Rev 0 19 March 2014
6-13
MD-80 MAINTENANCE MANUAL
ITEMNO.
ITEMS CK REQAPL
WEIGHT(LBS)
ARM
A NOSE COMPARTMENT
STATION 7 TO STATION 37
A-1 Antenna, Weather Radar - Bendix 2041446-0401 1 6.5 20
A-2 Drive Unit, Antenna - Bendix 2041444-0403 1 22.0 30
A-3 Radome Shell - 1009100-3 1 34.0 30
A-4 Antenna, Glide Slope - Collins 522-0700-023 1 .5 33
Rev 0 19 March 2014
6-14
MD-80 MAINTENANCE MANUAL
ITEMNO.
ITEMS CK REQAPL
WEIGHT(LBS)
ARM
B FORWARD ACCESSORY AND CREW COMPARTMENTS
STATION 37 TO STATION 160
FORWARD ACCESSORY COMPARTMENT
B-1 Gyro, Directional #1 - Sperry 2588302-4 1 9.0 45
B-2 Transformer Rectifier - G.E. 6RW176YN3 2 11.2 47
B-3 Inverter, Static - Leland ASH734-1 1 12.8 49
B-4 Transformer Rectifier - G.E. 6RW176YN3 2 11.2 54
B-5 Gyro, Directional #2 - Sperry 2588302-4 1 9.0 56
B-6 Transceiver Radar - Bendix 2041217-0414 1 26.8 63
B-7 Gyro, Vertical - Sperry 2587335-113 3 14.7 63
B-8 Inverter, Standby Horizon - TSG420-102 1 1.4 71
B-9 Gyro Switching Unit - Butler 001111-101 1 7.0 67
CREW COMPARTMENT
B-11 Control, Weather Radar - Bendix 2041223-0412 1 1.5 91
B-12 Clock, 2-Inch - Aerosonic 87000-1115 2 .6 93
B-13 Microphone, Pilot’s - Telex 63999-002 2 .5 110
B-14 Handset - Telex 63274-008 1 .8 130
B-15 Headset - Pilot’s - Telex 64060-001 2 .9 130
B-16 Seat, Pilot’s - IPECO 3A071-0005 & -0006 2 46.4 129
B-17 Belt, Seat, Pilot’s - Pacific 0108900 2 1.9 129
B-19 Regulator, 02 Diluter - Demand, Pilot’s 2 2.7 111
Bendix 29261-7E-A1
B CREW COMPARTMENT
STATION 90 TO STATION 160
B-20 Mask, O2, w/ Microphone, Pilot’s-Puritan 114426-21 2 2.8 140
B-21 Smoke Goggles - Puritan 118072-01 3 .3 141
B-22 Regulator, O2 Diluter - Demand, Observer 1 2.7 144
Bendix 29261-7E-A1
B-23 Mask, O2, w/ Mic & Switch, Obs - Puritan 114426-21 1 2.8 145
B-24 Cylinder, O2 Crew 48 cu. ft. - Scott 801307-20 1 21.7 145
B-25 Regulator, Crew O2 - 5749 1 .8 145
B-26 Fire Extinguisher, Halon - Halon 1211 1 3.5 145
B-28 Headset, Observer - Telex 4630 1 .9 147
B-29 Axe, Emergency - Reuleta 42D8331 1 2.5 147
B-30 Seat, Observer - DAC 55914552-507 1 15.0 158
B-31 Harness, Shoulder, Observer - Pacific 1101440 1 .5 157
B-32 Belt, Observer Seat - Pacific 1101011 1 1.4 157
B-33 Magnetic Compass 1 .5 140
Rev 0 19 March 2014
6-15
MD-80 MAINTENANCE MANUAL
B-34 Lifevest, Crew - Air Cruisers P0723E105P 3 1.5 141
B-35 Control Display Unit - Delco 965-0608-001 1 7.0 121
B-36 Printer, ACARS - Datametrics 109500-105 1 9.0 135
B-37 Carpet, Cockpit - 11.0 128
ITEMNO.
ITEMS CK REQAPL
WEIGHT(LBS)
ARM
Rev 0 19 March 2014
6-16
MD-80 MAINTENANCE MANUAL
ITEMNO.
ITEMS CK REQAPL
WEIGHT(LBS)
ARM
C PASSENGER COMPARTMENT
STATION 160 TO STATION 1360
C-1 Galley No. 1 (No Inserts) - Nordskog 1-657 1 125.4 157
C-1E Waste Container - Nordskog 67144 1 10.0 156
C-2 Light, Portable Emergency - DAC 5917239 1 1.5 157
C-3 Handset, Cabin Communication - Telex 63274-008 1 .8 160
C-4 Seat, Attendant - Jamco 5954612-503 1 20.0 163
C-5 Harness, Shoulder 2 2.3 163
C-6 Headrest 1 6.3 162
C-7 Lifevest, Air Cruisers P0723E105P 2 1.5 163
C-8 Slide - Air Cruisers D29982-103 2 27.6 180
C-10 Curtain, G1 to G2 1 3.5 180
C-11 Flashlight & Bracket - DME P2-07-0001-201S 2 1.3 161
Rev 0 19 March 2014
6-17
MD-80 MAINTENANCE MANUAL
ITEMNO.
ITEMS CK REQAPL
WEIGHT(LBS)
ARM
D WING COMPARTMENT
CENTER, LEFT & RIGHT
D-1 Strut, Main Landing Gear 2 485.0 971
Cleveland Pneumatic
D-2 Wheels, Main Landing Gear - 44.5 x 16.5-20 4 138.0 967
Bendix 2608891
D-3 Tire, Main Landing Gear - 44.5 x 16.5-20 4 190.0 967
Goodyear
D-4 Brakes, Main Landing Gear 4 309.0 967
Bendix 2608892
D-5 Spray Deflector Main Gear 2 18.5 989
Rev 0 19 March 2014
6-18
MD-80 MAINTENANCE MANUAL
ITEMNO.
ITEMS CK REQAPL
WEIGHT(LBS)
ARM
E TAIL COMPARTMENT
STATION 1138 TO STATION 1633
E-1 Fixed Fire Extinguisher, 2 req. - Walter Kidde
Container - 34400001 / 3934463 2 22.5 1353
Discharge Valve 6 .3 1353
Cartridge - 30903827 6 .1 1353
E-2 APU, Gas Turbine - AiResearch GTCP85-98DHF 1 340.0 1366
E-3 Generator, APU - Westinghouse 976J252-6 1 86.0 1366
E-4 Oil, APU Usable & Unusable - 8.7 1378
E-5 Air Conditioning Unit, Primary - AiResearch 2 34.8 1400
2202180-1
E-6 Air Conditioning Unit, Secondary - AiResearch 2 67.0 1400
184060-3-2 Right / 194110-1 Left
E-9 Tail Cone Assy, HF - DAC 5940163-507 1 108.3 1566
Rev 0 19 March 2014
6-19
MD-80 MAINTENANCE MANUAL
ITEMNO.
ITEMS CK REQAPL
WEIGHT(LBS)
ARM
F LOWER FORWARD FUSELAGE
STATION 110 TO STATION 218
F-1 Tire, Nose Landing Gear - 26 x 6.6 2 33.1 98
F-2 Wheel, Nose Landing Gear - 26 x 6.6 2 27.7 98
F-3 Strut, NLG - Cleveland Pneumatic - 5910448-531 1 183.0 100
F-4 Spray Deflector, NLG - 5930194-505 1 37.5 110
CENTER FORWARD
F-5 Charger, Battery - URDC 203BC102-1 1 12.0 115
F-6 Batteries - G.E. 023964-000 2 46.5 127
FWD RIGHT RADIO RACK
F-7 Transceiver, VHF #3 - King 622-1181-006 1 14.0 120
F-8 Transceiver, VHF #1 - King 622-1396-206 1 14.0 125
F-9 Transceiver, VHF #2 - King KTR 9100A 1 14.0 130
F-10 Symbol Generator #2 - Sperry 4055900-905 1 19.8 138
F-11 Receiver VOR/ILS NAV #2 - Bendix 2041234-3401 1 12.3 143
F-12 Aural Warning - MDEC HO5A0035-4 1 9.8 148
F-14 Receiver, ADF #2 - Bendix 2041168-7501 1 8.6 155
F-15 Marker Beacon - Collins 522-2996-011 1 3.0 125
F LOWER FORWARD FUSELAGE
STATION 110 TO STATION 218
F-17 D to A Syncro Converter Transmagnetics 5181-1PB 1 3.8 134
F-18 D.F.G.C.S. #2 - Sperry 4034241-930 1 28.8 141
F-19 P.A. Amplifier - Pacific Electro Dynamics 255-8 1 5.5 150
F-20 Computer, Air Data #2 - Honeywell HG280D80 1 13.0 155
F-21 Flight & Service Interphone Amplifier 2 .7 120
Gables G3122B
F-22 SELCAL Dual Decoder - Motorola NA-1335B 1 3.5 124
F-23 Computer Stall Warn #2 - Sundstrand 965-0449-002 1 8.5 127
F-24 Compass Rack -2, Servo & Slaving Amplifier 1 3.2 130
Sperry 614937-10, 1783867-11 & 2585703
F-25 Servo Power Supply - Abbott Labs 813201 1 4.8 141
F-26 Computer, Stall Warn #1 - Sundstrand 965-0449-002 1 8.5 147
F-27 Cabin Press -1 - AiResearch 2117180-2 1 10.3 151
F-28 Cabin Press -2 - AiResearch 2117180-2 1 10.3 155
Rev 0 19 March 2014
6-20
MD-80 MAINTENANCE MANUAL
F LOWER FORWARD FUSELAGE
STATION 110 TO STATION 218
AFT RIGHT RADIO RACK
F-29 Control Box, Engine Syncro-Woodward 213729 1 2.0 165
F-30 Flight Data Acq Unit - Ham ED742951-7 1 17.5 196
F-31 ACARS Mgmt Unit - Sundstrand 965-0612-002 1 7.5 198
F-33 Proximity Switch Control - Eldec 8-336-5 Mod A 1 15.0 175
F-34 Auto Brake Computer - Hydroaire 42-809-3 1 4.5 202
F-35 Anti-Skid Control Box - Hydroaire 42-807 1 5.3 205
F-37 Isolation Module - Kratos 50793 1 1.0 209
EQUIP PANEL - AFT RIGHT RADIO RACK
F-39 Fuel Flow Power Supply #1 - Gani 8TJ88 - GAN4 1 2.0 197
F-40 Fuel Flow Power Supply #2 - Gani 8TJ88 - GAN4 1 2.0 202
F-41 Auto Spoiler Control - Hydroaire 42-091-3 1 2.5 207
F LOWER FORWARD FUSELAGE
STATION 110 TO STATION 218
AFT LEFT RADIO RACK
F-42 Receiver, VOR/ILS NAV #1 - Bendix 2041234-3401 1 12.3 180
F-43 Symbol Generator #2 - Sperry 4055900-905 1 19.8 185
F-44 Transceiver, DME-2 - King 066-1019-63 1 19.0 190
F-45 Transceiver, DME-1 - King 066-1019-63 1 19.0 195
F-46 Transponder, ATC-1 - King 066-01127-1101 1 8.9 203
F-48 Transponder, ATC-2 - King 066-1056-00 1 8.9 208
F-49 Adapter, ATC-2 - King 068-1011-00 1 4.5 208
F-50 Compass Rack -1, Servo & Slaving Amplifier 1 3.2 209
Sperry 614937-10, 1783867-11 & 2585703
F-51 Computer, Air Data #1 - Honeywell HG280D80 1 13.0 203
F-52 D.F.G.C.S. #1 - Sperry 4034241-971 1 28.8 183
F-53 Auto Spoiler - DAC 5935212-501F 1 8.0 177
F-54 Ground Proximity Computer-Sundstrand 965-0976-003
F-55 Air Data Switch Unit - Butler 001048-101 1 5.7 166
F-56 Performance Computer - Delco 7892551-011-010 1 28.0 175
ITEMNO.
ITEMS CK REQAPL
WEIGHT(LBS)
ARM
Rev 0 19 March 2014
6-21
MD-80 MAINTENANCE MANUAL
ITEMNO.
ITEMS CK REQAPL
WEIGHT(LBS)
ARM
G FORWARD CARGO COMPARTMENT
STATION 218 TO STATION 786
G-1 Transmitter Receiver, Radio Altimeter 2 20.3 664
G-2 Potable Water - 392.0 487
Rev 0 19 March 2014
6-22
MD-80 MAINTENANCE MANUAL
ITEMNO.
ITEMS CK REQAPL
WEIGHT(LBS)
ARM
K AFT CARGO COMPARTMENT
STATION 1007 TO STATION 1320
K-1 Battery Emergency Lights - Grimes 60-1177-9 1 6.1 1055
K-2 Recorder, Voice 1 21.5 1240
2100-1020-00
K-3 Flight Data Recorder 1 28.0 1243
2100-4042-00
Rev 0 19 March 2014
6-23
MD-80 MAINTENANCE MANUAL
ITEMNO.
ITEMS CK REQAPL
WEIGHT(LBS)
ARM
L NACELLE COMPARTMENT
L-1 Usable and Unusable Engine Oil - 126.5 1303
L-2 Started, Engine - AiResearch 383342-1-1 2 27.5 1320
L-3 Generator - Westinghouse 976J252-6 2 86.0 1328
L-4 Engine, Turbofan - Pratt & Whitney JT8D-219 2 4451 1334
L-5 CSD - Sundstrand 696233B 2 70.0 1318
Rev 0 19 March 2014
6-24
MD-80 MAINTENANCE MANUAL
ITEMNO.
ITEMS CK REQAPL
WEIGHT(LBS)
ARM
9 Peep Hole Covers 2 .3 990
10 RH Sidewall Panel - Ventral Stair 1 8.5 1364
12 Upper & Lower Cowl Doors, RH & LH Engine - 590.0 1338
13 MLG Links (Non-Productions) Cylindrical - 147.0 970
14 MLG Links (Production) + Attaching Parts - 137.7 137.7
15 Ceiling Panel - Cockpit Entry 1 2.5 158
16 Aft Pressure Bulkhead Door 1 111.0 1350
18 Closeout Panel, Fwd C/A Seat 1 1.0 160
19 Light Control - Center Console Cockpit 1 1.5 125
20 Audio Panel - Observer Cockpit 1 4.5 135
21 Closeout Panel - Aft Cockpit 1 3.0 147
22 Overhead Switch Light Panel 1 1.5 125
24 Closeout Panels - Center Console 4 .2 100
25 Proximity Switch Control - Eldec 8-336-OS MODA
ADJUSTMENT TO AS WEIGHT WEIGHT
Rev 0 19 March 2014
7-1
MD-80 MAINTENANCE MANUAL
CHAPTER: 7 RESERVED FOR FUTURE USE
Rev 0 19 March 2014
7-2
MD-80 MAINTENANCE MANUAL
Intentionally Left Blank
Rev 0 19 March 2014
8-1
MD-80 MAINTENANCE MANUAL
CHAPTER: 8 RESERVED FOR FUTURE USE
Rev 0 19 March 2014
8-2
MD-80 MAINTENANCE MANUAL
Intentionally Left Blank
Rev 0 19 March 2014
9-1
MD-80 MAINTENANCE MANUAL
CHAPTER: 9 RESERVED FOR FUTURE USE
Rev 0 19 March 2014
9-2
MD-80 MAINTENANCE MANUAL
Intentionally Left Blank
Rev 0 19 March 2014
10-1
MD-80 MAINTENANCE MANUAL
CHAPTER: 10 AIRWORTHINESS LIMITATIONS INSTRUCTIONS,CERTIFICATION MAINTENANCE REQUIREMENTS,SPECIAL COMPLIANCE ITEMS
10.1 Introduction
Chapter 10 of the MD-80 Maintenance Planning Document lists tables that reference the Airworthiness Limitation Instructions (ALI), Certification Maintenance Requirements (CMR), and Special Compliance Items (SCI). This section is not the authorizing/controlling document. Operators shall use Chapter 10 as reference only.
Specific requirements are found in the latest revision of the controlling documents.
• MD-80 Certification Maintenance Requirements, Rev N, 07 Apr 2004 (Report No. MDC-J1271).
• Twinjet Special Compliance Item Report, Rev J, 26 Jan 2010 (Report No. MDC-92K9145).
10.2 Notes: Main Cargo Door Modification (STC ST02434LA)
1. Scheduled maintenance tasks for the main cargo door modification can be found in Chapter 12.
10.3 Scope
The scheduled maintenance requirements described in this chapter result from the MD-80 certification activities with the U.S. Federal Aviation Administration (FAA). Accordingly, the FAA approved Airwor-thiness Limitations and Certification Maintenance Requirements document is cross referenced in the MD-80 Type Certificate Data Sheet. These maintenance actions are mandatory. The Airworthiness Limitations Instructions report is FAA approved and specifies maintenance required under Title 14 Code of Federal Regulations (CFR) § 43.16 and 91.403 unless an alternative program has been FAA approved.
• AIRWORTHINESS LIMITATIONS INSTRUCTIONS (ALI) - SYSTEMS INSPECTIONS.
The Airworthiness Limitations Instructions (ALI) - systems inspections, as found in the Special Com-pliance Items (SCI) report, are scheduled maintenance tasks that may only be revised by the Long Beach FAA ACO. Principal Airworthiness Inspectors (local regulatory authority) may not change these requirements or the intervals associated with these requirements.
• CERTIFICATION MAINTENANCE REQUIREMENTS (CMR).
These scheduled maintenance tasks may only be revised by the Long Beach FAA ACO. Principal Air-worthiness Inspectors (local regulatory authority) may not change these requirements or the intervals associated with these requirements.
• SPECIAL COMPLIANCE ITEMS (SCI).
These scheduled maintenance tasks may only be revised by the Long Beach FAA ACO. Principal Air-worthiness Inspectors (local regulatory authority) may not change these requirements or the intervals associated with these requirements.
10.4 Airworthiness Limitations Instructions (ALI) - Systems
10.4.1 Fuel Systems Airworthiness Limitations
This section contains an FAA approved program of Airworthiness Limitation Instructions (ALIs) for oper-ators to incorporate into their maintenance program for this type of design to meet the new standards and assumptions introduced by § 25.981 and Special Federal Aviation Regulation (SFAR) No. 88. SFAR 88 Fuel Tank System Fault Tolerance Evaluation Requirements and Title 14 CFR 25.981 Fuel Tank Ignition Prevention require maintenance instructions, and control limitations for certain fuel tank critical design configurations.
Rev 0 19 March 2014
10-2
MD-80 MAINTENANCE MANUAL
NOTE: The auxiliary fuel tank installation has been shown to comply with CFR 25.981 at Amend-ment 25-102.
Paragraph 2(a) of SFAR 88 and Paragraph (b) of the new standard introduced by §25.981 requires certain design approval holders of Type Certificates (TCs) and Supplemental Type Certificates (STCs) of large transport airplanes to conduct a safety review of the fuel tank systems. The purpose of the safety review is to identify design features that may result in development of ignition sources in the fuel tank systems. Fuel System Airworthiness Limitations (ALIs) are mandatory maintenance actions required to ensure that unsafe conditions identified by the SFAR 88 safety review do not occur or are not introduced into the fuel tank system as a result of configuration changes, repairs, alterations, or deficiencies in the maintenance program throughout the operational life of the airplane. A critical fuel tank ignition source prevention fea-ture may exist in the fuel system and its related installation or in systems that, if a failure condition were to develop, could interact with the fuel system in such a way that an unsafe condition would develop without this limitation. Strict adherence to configuration, methods, techniques, and practices as prescribed is required to ensure compliance with the Critical Design Configuration Control Limitation (CDCCL). Any use of parts, methods, techniques or practices not contained in the applicable CDCCL must be approved by the Long Beach FAA ACO or applicable regulatory agency.
10.5 Certification Maintenance Requirements (CMR)
10.5.1 Selection of CMRs
In order to grant operators of the MD-80 an opportunity to participate in the evaluation and selection of CMRs in an integrated process with MRB tasks and intervals, a Certification Maintenance Coordination Committee (CMCC) was convened to review all of the MD-80 CMRs. The CMRs listed in this document are the result of applying the CMCC process as described in AC 25-19.
10.5.2 CMR Definition
As defined by AC 25-19, a CMR is a required periodic task, established during the design certification of the airplane as an operating limitation of the type certificate. CMRs usually result from a formal, numerical analysis conducted to show compliance with catastrophic and hazardous failure conditions. Additional notes concerning the definition of CMRs:
A CMR is intended to detect safety-significant latent (hidden) failures that would, in combination with one or more specific failures or events, result in a hazardous or catastrophic failure condition.
It is important to note that CMRs are derived from a fundamentally different analysis process than the maintenance tasks and intervals that result from the Maintenance Steering Group (MSG-3) Analysis asso-ciated with Maintenance Review Board (MRB) activities. MSG-3 Analysis activity produces maintenance tasks that are performed for safety, operational, or economic reasons, involving both preventative mainte-nance tasks, which are performed before failure occurs (and are intended to prevent failures), as well as failure-finding tasks. CMRs, on the other hand, are failure finding tasks only, and exist solely to limit the exposure to otherwise hidden failures. Although CMR tasks are failure-finding tasks, use of potential fail-ure-finding tasks, such as functional checks and inspections, may also be appropriate.
CMRs are designed to verify that a certain failure has or has not occurred, and do not provide any preven-tative maintenance function. CMRs “restart the failure clock to zero” for latent failures by verifying that
List of Airworthiness Limitations Instructions (ALI) - Systems - Tasks
MPD No. ALI No. Task
Interval Applicability
Task DescriptionThres Repeat APL ENG
29-001-00 20-2 DET 5000 FH NOTE
5000 FH
NOTE
All All Detailed Inspection of the Auxiliary Hydraulic Pump Power Feeder Wiring (ALI 20-2) Interval Note: MDC-92K9145
Rev 0 19 March 2014
10-3
MD-80 MAINTENANCE MANUAL
the item has not failed, or cause repair if it has failed. Because the exposure time to a latent failure is a key element in the calculations used in a safety analysis performed to show compliance with 14 CFR 25.1309, limiting the exposure time will have a significant effect on the resultant overall failure probability of the system. The CMR Task Interval should be designated in terms of flight hours, cycles, or calendar time, as appropriate.
The type certification process assumes that the airplane will be maintained in a condition of airworthiness at least equal to its certified or properly altered condition. The process described in AC 25-19 is not intended to establish normal maintenance tasks that should be defined through the MSG-3 Analysis pro-cess. Also, this process is not intended to establish CMRs for the purpose of providing supplemental mar-gins of safety for concerns arising late in the type design approval process.
CMRs should not be confused with required structural inspection programs that are developed by the type certificate applicant to meet the inspection requirements for damage tolerance, as required by 14 CFR 25.571 or 25.1529, Appendix H 25.4 (Airworthiness Limitations section). CMRs are to be developed and administered separately from any structural inspection program.
10.6 Post-Certification Changes to CMRs
Any post-certification changes to CMRs should be reviewed by the MD-80 CMCC and approved by the Long Beach FAA ACO:
Since the purpose of a CMR is to limit the exposure time to a given significant latent failure as part of an engineering analysis of overall system reliability, instances of a CMR task repeatedly finding that no fail-ure has occurred may not be sufficient justification for deleting the task or increasing the time between repetitive performances of the CMR task. In general, * CMRs are not good candidates for escalation under an operator’s reliability program. A CMR task change or interval escalation can only be made if world fleet service experience indicates that certain assumptions regarding component failure rates made early during the engineering analysis were overly conservative, and a recalculation of system reliability with revised failure rates of certain components reveals that the * CMR task or interval may be changed.
The introduction of a new CMR or any change to an existing CMR should be reviewed by the same pro-cess used during initial certification. It is important that operators be afforded the same opportunity to par-ticipate that they received during the original certification of the airplane, in order to allow the operators to manage their own maintenance programs.
In the event that later data provide sufficient basis for relaxation of a CMR (less restrictive actions to be required), the change may be documented by an FAA-ACO approved change to this CMR document.
If the requirements of an existing CMR must be increased (more restrictive actions to be performed), it will be implemented by a change to this CMR document and enforced by an FAA Airworthiness Directive (AD).
After initial aircraft certification, the only basis for adding a new CMR is in association with the certifica-tion of design changes.
A new CMR created as part of a design change should be part of the approved data for that change and added to this CMR document.
In the event that a CMR is revised, Boeing will document it by preparing a revision to this document that will be approved by the Long Beach FAA ACO. This revision will then be forwarded to all MD-80 opera-tors and the Long Beach FAA ACO offices.
Rev 0 19 March 2014
10-4
MD-80 MAINTENANCE MANUAL
10.7 Special Compliance Items (SCI)
10.7.1 Introduction
For some MD-80 system functions, compliance with SFAR 88 and Advisory Circular (AC) 25.981-1C require inspections for certain design configurations, using AC 25-19 “Certification Maintenance Require-ments (CMRs)” methodology as a guide.
Similarly, Airworthiness Limitation Instruction (ALIs) is a means of detecting safety significant condi-tions, potentially making the airplane noncompliant with SFAR 88 and 14 CFR 25.981(b). When an ALI detects such a condition, a maintenance action to correct it, is required.
The terms of the MD-80 Type Certificate are only valid when associated checks specified by these ALIs are performed within the time intervals specified. ALIs are equivalent to one-star CMRs (per AC 25-19):
The configuration control checks and intervals specified are mandatory and cannot be changed, esca-lated, or deleted without the approval of FAA Engineering of the Aircraft Certification Office having cognizance over the type design.
Temporary deviations from the ALI intervals are permitted within the limitations of Appendix D of the SCI report. While each ALI is included in this report, it is required that each ALI also be included in an appropriate document where it will be visible to airline personnel; therefore each ALI must be included in each Operator’s Maintenance Program. SFAR 88 established requirements for ALIs; it includes an imple-mentation schedule of changes to the operator’s maintenance program to manage compliance with these limitations and implementation of these checks.
For some MD-80 system functions, compliance with SFAR 88 and Advisory Circular (AC) 25.981-1C require inspections for certain design configurations, using AC 25-19 “Certification Maintenance Require-ments (CMRs)” methodology as a guide.
List of Certification Maintenance Requirements (CMR) - Tasks
MPD No. CMR No.
Task
Interval Applicability
Task DescriptionThres Repeat APL ENG
22-001-00 22-1.a OPC 450
FH
450
FH
ALL ALL Return-to-Service (RTS) Check of the Digital Flight Guidance (DFGS) Systems
Special Note: CMR No 22-1.a
22-002-00 22-1.b.1 GVI 10000
FH
10000 FH
ALL ALL General Visual Inspection of the Elevator Autopilot Servo Torque Limiter Dual Springs
Special Note: CMR 22-1.b.1
22-003-00 22-1.b.2 DET 10000
FH
10000 FH
ALL ALL Detailed Visual Inspection of the Elevator Autopilot Servo Torque Limiter Pushrod Assembly
Special Note: CMR No 22-1.b.2
27-003-00 27-1 OPC 2500
FH
2500 FH
ALL ALL Perform a take-off warning operational test, the flap handle/flap thumbwheel warning switch, horizontal
stabilizer green band switch and ground sensing relay functions are verified good.
Special Note: CMR No 27-1
22-004-00 34-3 OPC 2500
FH
2500 FH
ALL ALL Operational Check of the Thrust Cutback System
Special Note: CMR No 34-3
33-001-00 33-1 FNC 5000
FH
5000 FH
ALL ALL Perform a functional check of the auto air-condition-ing pack shut down and landing light retract system.
Special Note: CMR No 33-1
Rev 0 19 March 2014
10-5
MD-80 MAINTENANCE MANUAL
Similarly, Airworthiness Limitation Instruction (ALIs) is a means of detecting safety significant condi-tions, potentially making the airplane noncompliant with SFAR 88 and 14 CFR 25.981(b). When an ALI detects such a condition, a maintenance action to correct it, is required.
The terms of the MD-80 Type Certificate are only valid when associated checks specified by these ALIs are performed within the time intervals specified. ALIs are equivalent to one-star CMRs (per AC 25-19):
The configuration control checks and intervals specified are mandatory and cannot be changed, esca-lated, or deleted without the approval of FAA Engineering of the Aircraft Certification Office having cognizance over the type design.
Temporary deviations from the ALI intervals are permitted within the limitations of Appendix D of the SCI report. While each ALI is included in this report, it is required that each ALI also be included in an appropriate document where it will be visible to airline personnel; therefore each ALI must be included in each Operator’s Maintenance Program. SFAR 88 established requirements for ALIs; it includes an imple-mentation schedule of changes to the operator’s maintenance program to manage compliance with these limitations and implementation of these checks.
All maintenance and repair instructions provided by Boeing have been updated where required to ensure compatibility with these inspections.
10.7.2 Definition
Special Compliance Items (SCIs) are a means of notifying the FAA, operators, and others of critical design items that cannot be changed without violating the design intent, potentially making the airplane unsafe. For example, the SCI might require a repetitive check of pitot probe drains.
The terms of the MD-80 Type Certificate are only valid when the SCIs are performed within the time inter-vals specified. SCIs are equivalent to one star CMR’s, per Advisory Circular (AC) 25-19: the tasks and intervals specified are mandatory and cannot be changed, escalated, or deleted without the approval of FAA Engineering within the Aircraft Certification Office having cognizance over the type design.
Temporary deviations from the SCI intervals are permitted within the limitations of Appendix D of the SCI document.
While each SCI is included in this report, it is required that each SCI also be included in an appropriate document where it will be visible to airline personnel; therefore each SCI must be included in each Opera-tor's Maintenance Program.
The SCIs are in addition to the maintenance requirements established by the Maintenance Review Board activity and documented in the Maintenance Review Board Report. Inclusion of SCIs in the Special Com-pliance Items Report is only intended to limit the extension of task intervals for those portions of the MD-80 systems identified.
Rev 0 19 March 2014
10-6
MD-80 MAINTENANCE MANUAL
List of Special Compliance Items (SCI) - Tasks
MPD No. SCI No. Task
Interval Applicability
Task DescriptionThres Repeat APL ENG
24-001-00 24-1 DIS 3 Yr Note
3 Yr Note
All Note
All Discard the Emergency Power Switch (S1-148). (SCI 24-1)
Airplane Note: This task is applicable to aircraft equipped with EMER PWR switch P/N 103-2200.
Interval Note: An AMOC is available for recalcula-tion of the interval for replacing the Emergency
Power Switch, per SCI 24-1.
35-001-01 35-1 DIS 12 Yr Note
12Yr Note
All All Discard the Passenger Chemical Oxygen Generators.
Interval Note: Refer to Twinjet Special Compliance Report MDC-92K9145, SCI 35-1 for requirement
part number applicability and compliance.
Rev 0 19 March 2014
11-1
MD-80 MAINTENANCE MANUAL
CHAPTER: 11 RESERVED FOR FUTURE USE
Rev 0 19 March 2014
11-2
MD-80 MAINTENANCE MANUAL
Intentionally Left Blank
Rev 0 19 March 2014
12-1
MD-80 MAINTENANCE MANUAL
CHAPTER: 12 STC - INSTRUCTIONS FOR CONTINUED AIRWORTHINESS
12.1 Maintenance Planning Data Document Supplement for MD-80 Cargo Conversion (STC ST02434LA)
1. Purpose.
The “Supplemental Maintenance Planning Data (MPD) Document for MD-80 Cargo Conversion” is a sup-plement to the “Boeing MD-80 Maintenance Planning Data” document and is applicable to certain Boeing MD-80 airplanes converted from a passenger to a freighter configuration. The information contained in this supplemental MPD only applies to items, components and/or systems that have been modified or added and is not intended to duplicate data that is presented in the Boeing document.
The “Supplemental Maintenance Planning Data (MPD) Document for MD-80 Cargo Conversion,” Doc. No. R-867, is the “Principal Manual” as defined by FAR H25.4(b).
There are no special tools, special inspections, or special inspection techniques that are required by this supplemental maintenance program.
• Send communications about this section to:
Aeronautical Engineers, Inc
765 NW 54th ST. Miami, FL 331667
E-mail: [email protected]
This section provides Instructions for Continued Airworthiness contained in the Maintenance Planning Data Document Supplement for MD-80 Cargo Conversion, Aeronautical Engineers, Inc. document R-867, and is in compliance with FAR 25.1529.
The data contained herein is applicable to all Boeing MD-80 aircraft converted from passenger to freighter by Aeronautical Engineers, Inc. and designated MD-80SF.
Figure 12-A: Systems Maintenance Program Example Page
Rev 0 19 March 2014
12-2
MD-80 MAINTENANCE MANUAL
2. Page Format System Maintenance Program.
Column Explanation
MPD ITEM NUMBER No changes to this explanation. See Boeing MD-80 Maintenance Planning Data document.
CAT No changes to this explanation. See Boeing MD-80 Maintenance Planning Data document.
TASK No changes to this explanation. See Boeing MD-80 Maintenance Planning Data document.
INTERVAL No changes to this explanation. See Boeing MD-80 Maintenance Planning Data document.
ZONE No changes to this explanation. See Boeing MD-80 Maintenance Planning Data document.
ACCESS No changes to this explanation. See Boeing MD-80 Maintenance Planning Data document.
APPLICABILITY APL No changes to this explanation. See Boeing MD-80 Maintenance Planning Data document.
APPLICABILITY ENG No changes to this explanation. See Boeing MD-80 Maintenance Planning Data document.
MAN-HOURS No changes to this explanation. See Boeing MD-80 Maintenance Planning Data document.
TASK DESCRIPTION No changes to this explanation. See Boeing MD-80 Maintenance Planning Data document.
Rev 0 19 March 2014
12-3
MD-80 MAINTENANCE MANUAL
MPD
Item
No.
Task Interval Zone Access
Applicability
Man-
Hours
Task Description
APL ENG
AE-26-030-01 GVI 1A 58 ALL ALL 0.10 Perform a General Visual Inspection of the smoke detectors in Main Cargo Compartment ceiling for security and condition.
AE-29-050-01 SVC 1A 46 ALL ALL 0.10 Service MCD Hydraulic Reservoir to proper fluid level.
AE-29-050-02 DET 1C 46
58
NOTE ALL ALL 0.25 Perform a Detailed Inspection of all of the MCD hydraulic components, tubing and fittings for leaks, and security.a. Hydraulic Tank.b. Electric Motor/Pump.c. Selector Valve.d. Hand Pump.e. Sequence Valve Manifolds
(four).f. Holding Valves (two).g. Hydraulic hoses.
ACCESS NOTE: Remove MCD Collective Locking Cover and LHS and RHS Access Covers. Remove Main Deck ceiling panels aft of 9G barrier to MCD.
AE-29-050-03 DET 1C 58 ALL ALL 0.10 Perform a Detailed Inspection of the MCD Lift Actuators for leaks, align-ment, condition and security.
AE-29-050-04 DET 1C 58 ALL ALL 0.10 Perform a Detailed Inspection of the MCD Lift Actuators upper support fittings, lift linkages, rod ends, pivot blocks, and attach fittings for align-ment, and missing, loose, bent, or broken bolts or pins, and for condi-tion, security.
AE-29-050-05 DET 1C 58 ALL ALL 0.10 Perform a Detailed Inspection of the MCD Lift Actuator hydraulic hoses and tubing for leaks, deterioration, and security.
Rev 0 19 March 2014
12-4
MD-80 MAINTENANCE MANUAL
MPD
Item
No.
Task Interval Zone Access
Applicability
Man-
Hours
Task Description
APL ENG
AE-29-050-06 DET 1C 58 NOTE ALL ALL 0.10 Perform a Detailed Inspection of the MCD Torque Tube Actuator, attach fittings, latch linkages, and rod ends for condition, security, and lubrica-tion.
ACCESS NOTE: Remove MCD Collective Locking Cover.
AE-29-050-07 DET 1C 58 NOTE ALL ALL 0.10 Perform a Detailed Inspection of the MCD Latch Lock Pin (Gang Bar) Actuator for leaks, condition and security.
ACCESS NOTE: Remove MCD Collective Locking Cover.
AE-29-050-08 DIS 1C 46 ALL ALL 0.25 Replace the MCD Hydraulic System filters (two) located on the MCD Hydraulic Panel.
AE-29-050-09 FNC 1C 58 NOTE ALL ALL 2.00 Bench Check MCD pressure relief valves (installed on Sequence Valve Manifolds) (four) located on the MCD, check for the proper pressure setting as per OHM R-4374.a. Torque Tube Open valve.b. Torque Tube Close valve.c. Lock Pin Close valve.d. Door Open valve.
ACCESS NOTE: Remove MCD access covers.
AE-32-080-01 GVI 1A 55
56
ALL ALL 0.25 Perform a General Visual Inspection of Secondary Main Landing Gear switches and wire routing in wheel well, for security and condition.
AE-35-020-01 FNC 2C 44
46
ALL ALL 0.05 Functional Check of the Passenger Oxygen System using Automatic Mode (Aneroid Switch).
AE-35-020-02 OPC 2C 44
46
ALL ALL 0.03 Operational Check of the Passenger Oxygen System using manual Eject Switch.
Rev 0 19 March 2014
12-5
MD-80 MAINTENANCE MANUAL
MPD
Item
No.
Task Interval Zone Access
Applicability
Man-
Hours
Task Description
APL ENG
AE-52-031-01 GVI 3 DY 50
58
ALL ALL 0.25 Perform a General Visual Inspection of the MCD pressure seal, with MCD open:a. Inspect the MCD edges for
nicks or deformations, which may impede or prohibit pressur-ization.
b. Inspect the MCD seal for abra-sions or cuts which may pro-hibit pressurization.
AE-52-031-02 GVI 1A 58 ALL ALL 0.05 Perform a General Visual Inspection of the MCD link assemblies for bending and obvious wear.
AE-52-031-03 GVI 3 DY 58 ALL ALL 0.10 Perform a General Visual Inspection of the MCD latch assemblies for obvious wear, damage and distor-tion.
AE-52-031-04 GVI 1A 58 ALL ALL 0.10 Perform a General Visual Inspection of the MCD hydraulic system, actu-ators, valves, tubing and hydraulic panel components for leaks, chafing or wear.a. Main Lift Actuators.b. Collective Locking (Gang Bar)
Actuator.c. Torque Tube Actuator.d. Hydraulic Plumbing.
NOTE: It is not necessary to remove liner or access panels. MCD can be open or closed.
AE-52-031-05 GVI 3 DY 58 ALL ALL 0.05 Perform a General Visual Inspection of the hydraulic hoses between the top of the MCD and upper jamb for cuts, leaks, wear, or signs of abra-sion.
AE-52-031-06 GVI 3 DY 58 ALL ALL 0.05 Perform a General Visual Inspection of the electrical harnesses between the top of the MCD and upper jamb for cuts, wear, or signs of abrasion.
Rev 0 19 March 2014
12-6
MD-80 MAINTENANCE MANUAL
MPD
Item
No.
Task Interval Zone Access
Applicability
Man-
Hours
Task Description
APL ENG
AE-52-031-08 GVI 1A 58 ALL ALL 0.25 Perform a General Visual Inspection of the MCD latching, locking and vent door mechanisms for condition and wear.a. Torque Tube.b. Lock Pins.c. Latches.d. Collective Locking (Gang Bar).e. Vent Doors.
ACCESS NOTE: Remove MCD Collective Locking Cover.
AE-52-031-09 GVI 1A 58 NOTE ALL ALL 0.25 Perform a General Visual Inspection of the MCD hydraulic system, actu-ators, valves, tubing and hydraulic panel components for leaks, chafing or wear.a. Main Lift Actuators.b. Collective Locking Actuator.c. Torque Tube Actuator.d. Hydraulic Piping.e. Valves.
ACCESS NOTE: Remove center MCD access cover.
AE-52-031-10 LUB 1A 58 NOTE ALL ALL 0.50 Lubricate the required components with Mobil 28 Grease or equivalent (MIL-G-81322, DPM 5348, Boeing AMM Chap. 12-21-00).a. Latches.b. Links (Door lift and latch).c. Gang Bar.d. Lock Pins.e. Vent Door Assembly and Inter-
lock.f. Main Lift Actuator Pivot
Mounts and Supports.
ACCESS NOTE: Remove MCD Collective Locking Cover.
Rev 0 19 March 2014
12-7
MD-80 MAINTENANCE MANUAL
MPD
Item
No.
Task Interval Zone Access
Applicability
Man-
Hours
Task Description
APL ENG
AE-52-031-11 RST 1A 58 NOTE ALL ALL 0.25 Clean MCD lock pin and torque tube viewports of dust, grease and other contamination using soapy water, Permatex Plastic Cleaner, or equiva-lent cleaner safe for use on acrylics.
ACCESS NOTE: Remove MCD Collective Locking Cover.
AE-52-031-13 DET 1C 58 NOTE ALL ALL 0.50 Perform a Detailed Inspection of the MCD Seal and Seal Depressors for condition and security.
NOTE: MCD must be open.AE-52-031-14 DET 1C 58 NOTE ALL ALL 0.25 Perform a Detailed Inspection of the
MCD Latches and Latch Plates for condition and security.
ACCESS NOTE: Remove MCD Collective Locking Cover.
AE-52-031-15 DET 1C 58 NOTE ALL ALL 0.10 Perform a Detailed Inspection of the MCD Latch Lock Pins and Attach Plates for condition and security.
ACCESS NOTE: Remove MCD Collective Locking Cover.
AE-52-031-16 DET 1C 58 NOTE ALL ALL 0.10 Perform a Detailed Inspection and adjust for proper operation the MCD Collective Locking (Gang Bar) ball plungers and detents, REF AEI AMM 52-33-05. Verify that ball plungers retain bar in locked posi-tion.
ACCESS NOTE: Remove MCD Collective Locking Cover.
AE-52-031-17 DET 1C 58 NOTE ALL ALL 0.10 Perform a Detailed Inspection of the MCD Vent Door assemblies, cable attachments and Vent Door hold open springs for corrosion, cracks, indication of deterioration, loose or missing fasteners, and security.
ACCESS NOTE: Remove MCD LHS and RHS Access Covers.
Rev 0 19 March 2014
12-8
MD-80 MAINTENANCE MANUAL
MPD
Item
No.
Task Interval Zone Access
Applicability
Man-
Hours
Task Description
APL ENG
AE-52-031-18 DET 1C 58 NOTE ALL ALL 0.10 Perform a Detailed Inspection of the MCD Vent Door cables for broken wire strands, damage to sheathing, loose or missing fasteners and secu-rity.
ACCESS NOTE: Remove MCD Collective Locking Cover and LHS and RHS Access Covers.
AE-52-031-19 DET 1C 58 NOTE ALL ALL 0.10 Perform a Detailed Inspection of the MCD switches and wiring for condi-tion and security.
ACCESS NOTE: Remove MCD Collective Locking Cover and MCD Access Covers.
AE-52-031-20 OPC 1C 58 ALL ALL 0.25 Perform a Operational Check of wire harnesses crossing from the MCD to the Upper Jamb.a. Disconnect fwd crossover har-
ness and operate MCD through normal cycle. MCD and MCD Warning System should oper-ate normally.
b. Re-Connect fwd crossover har-ness and disconnect aft cross-over harness and operate MCD through normal cycle. MCD and MCD Warning System should operate normally.
c. Reconnect aft crossover har-ness.
AE-52-031-21 LUB 1A 50 ALL ALL 0.50 Lubricate the MCD hinge with LPS2 lubricant or equivalent lubricant meeting MIL-C-81309D.
AE-52-031-22 OPC 1A 58 ALL ALL 0.25 Perform a Operational Check of the MCD Latching, Locking and Vent Door Systems to insure MCD oper-ates properly.
Rev 0 19 March 2014
12-9
MD-80 MAINTENANCE MANUAL
MPD
Item
No.
Task Interval Zone Access
Applicability
Man-
Hours
Task Description
APL ENG
AE-52-071-01 OPC 3 DY 44
46
ALL ALL 0.10 Perform a Operational Check of the MCD Control and Warning System for proper operation to insure all of the switches and indicators are properly functioning. With MCD unlocked, unlatched and open, verify illuminated.a. “Main Cargo Door” Annunciator on
Overhead Annunciator Panel.b. “Main Cargo Door Armed” Annun-
ciator on Overhead Annunciator Panel.
c. “Cargo Door” warning light on MCD control panel.
d. “Vent Door Open” light on MCD control panel.
e. “Latch Lock Pins Not Engaged” light on MCD control panel.
f. “Latches Unlocked” light on MCD control panel.
g. “Hooks Unlocked” light on MCD control panel.
h. “Main Cargo Door Not Closed” light on MCD control panel With MCD closed, latched and locked.
i. Verify all indicators on MCD con-trol panel and on Overhead Annun-ciator panel are extinguished.
AE-52-071-02 OPC 1C 46
58
NOTE ALL ALL 0.25 Perform a Operational Check of Lock Pin Limit switches to verify that both provide indication to MCD Warning System. With MCD unlocked, unlatched and open:a. Disconnect aft Lock Pin switch
from terminal block TB-AE2, ver-ify “Latch Lock Pins Not Engaged” Indicator on MCD Control Box is illuminated.
b. Reconnect aft Lock Pin switch.c. Disconnect fwd Lock Pin switch
from terminal block TB-AE2, ver-ify “Latch Lock Pins Not Engaged” Indicator on MCD Control Box is illuminated.
d. Reconnect fwd Lock Pin switch.
ACCESS NOTE: Remove MCD Col-lective Locking Cover and MCD Access Covers.
Rev 0 19 March 2014
12-10
MD-80 MAINTENANCE MANUAL
MPD
Item
No.
Task Interval Zone Access
Applicability
Man-
Hours
Task Description
APL ENG
AE-52-071-03 OPC 1C 46
58
NOTE ALL ALL 0.25 Perform a Operational Check Vent Door switches to verify that both provide indi-cation to MCD Warning System. With MCD unlocked, unlatched and open:a. Disconnect aft Vent Door switch
from terminal block TB-AE2, ver-ify “Vent Door Open” Indicator on MCD Control Box is illuminated.
b. Reconnect aft Vent Door switch.c. Disconnect fwd Vent Door switch
from terminal block TB-AE2, ver-ify “Vent Door Open” Indicator on MCD Control Box is illuminated.
d. Reconnect fwd Vent Door switch.
ACCESS NOTE: Remove MCD Col-lective Locking Cover and MCD Access Covers.
AE-52-071-04 OPC 1C 46
58
NOTE ALL ALL 0.25 Perform a Operational Check of MCD Not Closed switches to verify that both provide indication to MCD Warning System. With MCD unlocked, unlatched and open:a. Disconnect aft MCD Not Closed
switch from terminal block TB-AE2, verify “Main Cargo Door Not Closed” Indicator on MCD Control Box is illuminated.
b. Reconnect aft MCD Not Closed switch.
c. Disconnect fwd MCD Not Closed switch from terminal block TB-AE2, verify “Main Cargo Door Not Closed” Indicator on MCD Control Box is illuminated.
d. Reconnect fwd MCD Not Closed switch.
ACCESS NOTE: Remove MCD Col-lective Locking Cover and MCD Access Covers.
Rev 0 19 March 2014
12-11
MD-80 MAINTENANCE MANUAL
MPD
Item
No.
Task Interval Zone Access
Applicability
Man-
Hours
Task Description
APL ENG
AE-52-071-05 OPC 1C 46
58
NOTE ALL ALL 0.25 Perform a Operational Check of Latch Hook switches to verify that all provide indication to MCD Warning System. With MCD unlocked, unlatched and open:a. Disconnect Latch No. 3 and No. 4
Latch Hook switch from terminal block TB-AE6, verify “Hooks Unlocked” Indicator on MCD Con-trol Box is illuminated.
b. Reconnect Latch No. 4 Latch Hook switch.
c. Disconnect Latch No. 5 Latch Hook switch from terminal block TB-AE6, verify “Hooks Unlocked” Indicator on MCD Control Box is illuminated.
d. Reconnect Latch No. 3 Latch Hook switch.
e. Disconnect Latch No. 4 Latch Hook switch from terminal block TB-AE6, verify “Hooks Unlocked” Indicator on MCD Control Box is illuminated.
f. Reconnect Latch No. 4 and No. 5 Latch Hook switch.
ACCESS NOTE: Remove MCD Col-lective Locking Cover and MCD Access Covers.
AE-52-071-06 OPC 1C 46 ALL ALL 0.25 Check diodes inside MCD Control and Relay Box for short and failure open.a. Disconnect D-AE001 connector.b. Check diodes for short and failure
open:
Diode CR-1.
Diode CR-2.
Diode CR-3.
Diode CR-4.
Diode CR-5.
Diode CR-6.c. Re-connect D-AE001 connector.
Rev 0 19 March 2014
12-12
MD-80 MAINTENANCE MANUAL
MPD
Item
No.
Task Interval Zone Access
Applicability
Man-
Hours
Task Description
APL ENG
AE-52-071-09 OPC 1C 45
46
ALL ALL 0.50 Perform a Operational Check of MCD Ground Control Relay R-AE309. With aircraft in FLIGHT mode:a. Verify that relay R-AE309 is
de-energized.b. Verify that all normally open
contacts are open.c. Verify that power is not pro-
vided to Master Power Switch S-AE1 on MCD Control Box.
AE-52-071-07 OPC 1C 44
46
ALL ALL 0.25 Perform a Operational Check of MCD Master Power Relay R-AE4. With Master Power Switch S-AE1 in the ON position:a. Verify that “MAIN CARGO
DOOR ARMED” Annunciator on Overhead Annunciator panel is illuminate.
b. With Master Power Switch S-AE1 in the OFF position:i. Verify that “MAIN
CARGO DOOR ARMED” Annunciator on Overhead Annunciator panel is extin-guished.
ii. Verify that relay R-AE4 is de-energized.
iii. Verify that all normally open contacts are open.
AE-52-071-08 OPC 1C 44 ALL ALL 0.50 Perform an Operational Check of the MCD Aural Warning System. With MCD in open:a. Verify “MAIN CARGO
DOOR” Annunciator on Over-head Annunciator panel is illu-minated.
b. Advance left throttle to takeoff power, MCD Aural Warning horn should sound (fast-pulse) until throttle is pulled back.
c. Advance right throttle to takeoff power, MCD Aural Warning horn should sound (fast-pulse) until throttle is pulled back.
AE-53-051-01 RST 1A 58 ALL ALL 0.05 Clean floor drains, located aft of 9G barrier, remove any debris from drain.
Rev 0 19 March 2014
12-13
MD-80 MAINTENANCE MANUAL
12.2 Structural Maintenance Program
1. Scope.
This section of the Maintenance Planning Document (MPD) outlines the scheduled tasks for the Structural Maintenance Program. The supplement provided in this section shows the inspections that have been affected or created due to the Aeronautical Engineers, Inc. freighter modification. This program is designed to provide timely detection and repair of structural damage which may occur in the fleet during freighter operations. Detection of corrosion, stress corrosion, minor accidental damage and fatigue crack-ing by visual and/or Non-Destructive Test (NDT) procedures is considered. Major accidental damage such as that caused by bird strike or large ground handling equipment is considered readily detectable and visi-ble signs such as fuel leaks, loose fasteners, loss of cabin pressure, etc., continue to be an essential part of the Structural Inspection Program. This baseline program is intended to serve as a guide for airlines to develop individual maintenance programs. The structural tasks listed herein constitute minimum inspec-tion requirements for all MD-80SF airplanes. Notes applicable to the Structural Maintenance Program are followed by explanations of the operating rules, age exploration program, supplemental structural inspec-tion program, reporting of structural inspection tasks, and the page format.
2. Fatigue Related Inspection Program.
Where the initial scheduled maintenance program does not ensure timely detection of potential fatigue damage in a structural item, supplemental fatigue related inspections will be required and are listed in AEI MD-80SF MCD & Surround Skin Supplemental Structural Inspection Document, Report SIE-367- 601. These inspections must be accomplished prior to reaching the fatigue task threshold.
3. Corrosion Prevention and Control Program.
Inspection requirements are determined on the basis of continual maintenance to preserve or restore the inherent corrosion preventive measures and structural surface finishes. Should corrosion be detected or should the corrosion inhibiting compound exhibit signs of deterioration during the performance of a struc-tural task, the Boeing Corrosion Control Handbook (CCH) - MDC K0805 should be referred to for appro-priate corrective action.
The Corrosion Prevention and Control Program (CPCP) is included as part of the Structural Inspection Program contained in this section. The objective of the CPCP is to control corrosion found on all structure listed in the Structural Inspection Program to Level 1 or better.
See Boeing MD-80 Maintenance Planning Data document for the CPCP Basic Task.
4. Reporting Results of Structural Inspection.
Reports of structural significant defects, as defined by the FAA Service Difficulty Reporting (SDR) pro-cess, shall be submitted by operators who are operating under FAA regulations.
In addition to the above, all cracks found during the supplemental structural inspections shall be reported within ten (10) days to Aeronautical Engineers using the Discrepant Structure Report form. Refer to AEI MD-80SF MCD & Surround Skin Supplemental Structural Inspection Document, Report SIE-367- 601, for the required report form (any suitable alternative which contains the same information may be used).
Rev 0 19 March 2014
12-14
MD-80 MAINTENANCE MANUAL
Figure 12-B: Structural Maintenance Program Example Page
Rev 0 19 March 2014
12-15
MD-80 MAINTENANCE MANUAL
5. Page Format Explanation.
Column Explanation
MPD ITEM NUMBER No changes to this explanation. See Boeing MD-80 Maintenance Planning Data document.
TASK No changes to this explanation. See Boeing MD-80 Maintenance Planning Data document.
INTERVAL No changes to this explanation. See Boeing MD-80 Maintenance Planning Data document.
ZONE No changes to this explanation. See Boeing MD-80 Maintenance Planning Data document.
ACCESS No changes to this explanation. See Boeing MD-80 Maintenance Planning Data document.
APPLICABILITY APL No changes to this explanation. See Boeing MD-80 Maintenance Planning Data document.
APPLICABILITY ENG No changes to this explanation. See Boeing MD-80 Maintenance Planning Data document.
MAN-HOURS No changes to this explanation. See Boeing MD-80 Maintenance Planning Data document.
TASK DESCRIPTION No changes to this explanation. See Boeing MD-80 Maintenance Planning Data document.
Rev 0 19 March 2014
12-16
MD-80 MAINTENANCE MANUAL
Figure 12-C: Structural Maintenance Program Tasks
MPD
Item
No.
C
A
T
Task Interval Zone Access
Applicability
Man-
Hours
Task Description
APL ENG
AE-52-031-07 GVI 1A 50
58
ALL ALL 0.50 EXTERNAL-GENERAL VISUAL: MCD and MCD Surround Perform a General Visual Inspection of both the interior and exterior of the MCD for cracks, broken, missing or loose fasten-ers. a. MCD and MCD surround structurE.b. MCD exterior skin.c. MCD inner skin.
NOTE: Removal of access covers not required.
AE-52-031-12 DET 1C 50
58
NOTE ALL ALL 2.00 EXTERNAL & INTERNAL - DETAILED: Main Cargo Door (MCD) Perform a Detailed Inspection of the MCD for corrosion, cracks, loose and missing fasteners, and security.
Check:a. MCD Upper Beam.b. MCD Lower Beam.c. MCD Side Beams.d. MCD Main Beams.e. Intercostals.f. Latch Plates.g. Inner skin.h. Outer skin and splices ACCESS.
NOTE: Remove MCD collective locking cover and MCD access covers.
AE-53-037-01 DET 1C 51
53
57
58
NOTE ALL ALL 4.00 INTERNAL - DETAILED: Floor beams Perform a Detailed Inspection of floor beams and floor beam reinforcements from FS218 to FS1309 for corrosion, cracking, loose or missing fasteners and security. Check:a Floor beams.b. Floor beam vertical stiffeners.c. Floor beam reinforcement straps
ACCESS.
NOTE: Remove lower cargo com-partment ceiling lining and floor panels in overwing area.
AE-53-037-02 DET 1C 58 NOTE ALL ALL 4.00 INTERNAL - DETAILED: Seat Tracks Perform a Detailed Inspection of main deck seat tracks from FS218 to FS1309 for corrosion, cracks, loose or missing fasteners.
ACCESS NOTE: Inspect seat track area visible in Main Cargo Compart-ment.
Rev 0 19 March 2014
12-17
MD-80 MAINTENANCE MANUAL
MPD
Item
No.
C
A
T
Task Interval Zone Access
Applicability
Man-
Hours
Task Description
APL ENG
AE-53-050-01 GVI 3 DY 58 ALL ALL 0.10 EXTERNAL - GENERAL VISUAL: MCD Spools and Latch Plates Per-form a General Visual Inspection of the MCD lower jamb area for obvious wear, damage and distortion.a. Spools.b. Latch Plate Assemblies.
AE-53-050-02 GVI 1A 50
58
ALL ALL 0.50 EXTERNAL: GENERAL VISUAL: MCD Surround Perform a General Visual Inspection of the MCD sur-round for cracks, broken, missing or loose fasteners.a. MCD surround skin and doublers,
externally.b. Upper Jamb and inner skin c
Lower Jamb.c. Forward and Aft Jamb, frames
and inner skin.
AE-53-050-03 DET 1C 58 NOTE ALL ALL 1.50 INTERNAL-DETAILED: MCD Fwd and Aft Jambs Perform a Detailed Inspection of the Forward and Aft Jambs of the MCD opening for corro-sion, cracks, loose and missing fasten-ers, and security. Check:a. Forward and Aft Jamb Frames at
FS389, FS397, FS533, FS541 from L-4L to L-18L.
b. Intercostals between FS389 and FS397, and between FS533 and FS541, from L-4L to L-18L.
c. Stringer Splices between FS370 and FS389, and between FS541 and FS560, from L-4L to L-18L.
d. Attach Fittings to Upper & Lower Beam at FS389, FS397, FS533 and FS541.
ACCESS NOTE: Remove access covers in MCD Forward and Aft Jambs.
NOTE: Take special note when inspecting areas at and around For-ward and Aft Jambs for loose or missing fasteners and damage.
Rev 0 19 March 2014
12-18
MD-80 MAINTENANCE MANUAL
MPD
Item
No.
C
A
T
Task Interval Zone Access
Applicability
Man-
Hours
Task Description
APL ENG
AE-53-050-04 DET 1C 50
58
ALL ALL 2.00 EXTERNAL & INTERNAL - DETAILED: MCD Surround Skins Perform a Detailed Inspection of the MCD Surround Skins and Doublers for corrosion, cracks, loose and miss-ing fasteners, and security. Check:a. Upper Skins, Doublers and splices
between FS360 and FS588, from L-2R to L-6L.
b. Lower Skins, Doublers and splices between FS360 and FS588, from L-16L to L-26L.
c. Forward Skins, Doublers and splices between FS360 and FS397, from L-6L to L-16L.
d. Aft Skin, Doublers and splices between FS533 and FS588, from L-6L to L-16L.
NOTE: Take special note when inspecting areas at and around Lower and Upper Jamb and For-ward and Aft Jambs for loose or missing fasteners and damage.
AE-53-050-05 DET 1C 51 NOTE ALL ALL 2.00 INTERNAL - DETAILED: MCD Sur-round - Lower Perform a Detailed Inspection of the area below the MCD for corrosion, cracks, loose and miss-ing fasteners, and security. Check:a. Lower Jamb between FS370-
FS560, at L-18L.b. Frames between FS370 to FS560
and between L-18L to L-26L.c. Frame splices at FS389 and
FS541, between L-24L and L-26L.
d. Latch fittings between FS408 to FS522.
e. Floor Beam Attachment Splice Plates between FS370 to FS560 LHS.
ACCESS NOTE: Remove fwd bag-gage compartment liner on LHS in area of MCD Lower Jamb.
Rev 0 19 March 2014
12-19
MD-80 MAINTENANCE MANUAL
MPD
Item
No.
C
A
T
Task Interval Zone Access
Applicability
Man-
Hours
Task Description
APL ENG
AE-53-050-06 DET 1C 58 NOTE ALL ALL 1.50 INTERNAL - DETAILED: MCD Sur-round - Upper Perform a Detailed Inspection of the area above the MCD for corrosion, cracks, loose and miss-ing fasteners, and security. Check:a. Upper Jamb between FS351 to
FS579, at L-4L.b. Frames between FS370 to FS560
from L-4L to L-2R.c. Frame splices between FS389 and
FS541 from L-2R and L-4R.d. Intercostals between FS389 and
FS541 at L-2L and L-1.e. Cargo Door Actuator Brackets
between FS408 to FS427, and between FS503 to FS522.
ACCESS NOTE: Remove ceiling panels in area of MCD door.
AE-53-050-07 DET 1C 50 ALL ALL 1.00 EXTERNAL - DETAILED: MCD Hinge Perform a Detailed Inspection of the MCD Hinge for corrosion, cracks, and security, also check for loose or missing fasteners.
NOTE: No cracks are allowed in any portion of the hinge.
Rev 0 19 March 2014
12-20
MD-80 MAINTENANCE MANUAL
12.3 Zonal Inspection Program
1. Scope.
The Zonal Inspection Program includes a general visual of the general condition and security of attachment of the accessible systems and structures items contained in defined zones. This includes checks for degra-dation such as chafing of tubing, loose duct supports, wiring damage, cable and pulley wear, fluid leaks, electrical bonding, general condition of fasteners, cracked, chipped, or missing paint, inadequate drainage, etc., and general corrosion, not covered in the MSG-3 system and structures analysis. The zonal inspection is not intended as a quality assurance after maintenance check for determining proper reassembly of sys-tems, components, or structures.
Figure 12-D: Zonal Inspection Program Tasks
12.4 Supplemental Structural Inspection Items for MD-80 Aircraft Modifiedwith Freighter Conversion STC. No. ST02434LA(Fatigue Related Inspections)
1. Introduction.
This supplement contains changes and additions to McDonnell Douglas document L26–022. MD-80 Sup-plemental Inspection Document.
This supplement requires that additional supplemental structural inspections for particular aircraft be con-ducted for the Principal Structural Elements (PSEs) that are created by the passenger to freighter conver-sions of MD-80 aircraft using non-destructive inspection (NDI) techniques and procedures. Additionally, the existing PSEs that are affected by this conversion, 53.08.015, 53.08.037, 53.08.039, and 53.08.042 are required to be conducted at an increased frequency as compared with that originally specified by Douglas.
There is no changes to the inspection intervals for the empennage or wing PSEs.
There are mandatory reporting requirements found in Chapter 4. The form shell be completed after every inspection and returned to AEI, even if no cracking is found. Any cracks found shall be repaired in a method approved by the FAA. Contact cognizant engineering support.
2. Applicability.
The following aircraft are required to implement this supplement:
• All aircraft that have installed STC project No. ST02434LA.
MPD
Item
No.
Task Interval Zone Access
Applicability
Man-
Hours
Task Description
APL ENG
AE-52–800–04 GVI 1C 58 NOTE ALL ALL 0.50 INTERNAL - ZONAL (GV): MCD and Surrounding Door Jambs Zonal Inspec-tion:
Internal - MCD and Surrounding Door Jambs.
ACCESS NOTE: MCD open, covers removed.
Rev 0 19 March 2014
12-21
MD-80 MAINTENANCE MANUAL
The following PSEs have threshold inspections that are aircraft dependent:
• 53.80.003 — Fuselage Skin Panels from Longeron 3L to 3R, FS674-927.
• 53.80.004 — Fuselage Skin Splices from Longeron 5L to 5R, FS588 and FS759.
• 53.08.006 — Fuselage Frame to Floor Beam Joints Over Main Landing Gear, FS946-FS984.
• 53.80.016 — Fuselage Shin and Frames from 15 to 18, FS1041-FS1098.
• 53.80.019 — Forward Lower Cargo Door Jamb Corners.
Table below lists the total number of flights since conversion at which the threshold inspections, Nth, should be initiated for the respective PSEs.
3. Modification TO L26-022.
The following inspection instructions should be included with Douglas document L26-022, Supplementary Inspection Document for MD-80 airplanes that have incorporated STC No. ST124445LA-T. The threshold interval that is called out in the inspection instructions is the total number of flights since conversion at which the first inspection should be conducted except where noted above. The repeat interval is the incre-ment of flights for subsequent inspections to be conducted throughout the life of the aircraft.
For the purposes of this document, a visual inspection is defined in the Douglas Nondestructive Testing Standard Practices Manual (NDTSPM), MDC 93K0393, Part 09 Section 00. The definitions for high fre-quency eddy current (ETHF) and low frequency eddy current (ETLF) inspections can also be found in this document. The specific references for these inspection methods are shown in the table below. This table is applicable to all ETHF and ETLF inspections called out by the method numbers on the following pages. Set up calibration for ETLF inspections shall be a 0.20 inch crack reference and verify a signal-to-noise ratio of 3:1 or better.
Figure 12-E: Douglas NDTSPM, MDC 93K0393, Part 06 Inspection MethodsReference Table
NOTE: Complete an internal visual inspection, as defined above, on the main cargo door and surrounding fuselage skin whenever the cargo compartment lining is removed. Internal access to the skin can be gained directly or through the inner skin lightening holes where applicable.
The items below are a list of items from report SIE-367-601. This list is for reference use only and when there are any discrepancies between this document and report SIE-367-601, report SIE-367-601 will be considered the authority.
Aircraft S/N Flights at Conversion
Nth
53.80.003
Nth
53.80.004
Nth
53.80.006
Nth
53.80.016
Nth
53.80.019
49470 34,732 49,237 63,725 66,946 71,376 51,662
Method Inspection Section Subject No.
1 ETHF surface and filled holes
10 01 001
2 ETHF open hole 10 01 003
.3 ETHF at edge of cut-outs
10 01 010
4 ETLF 10 02 001
Rev 0 19 March 2014
12-22
MD-80 MAINTENANCE MANUAL
Figure 12-F: Supplemental Structural Inspection Tasks for MD-80 AircraftModified with Freighter Conversion STC No. ST02434LA(Fatigue Related Inspections)
PSE
Item
Number
P
G
M
Access
Interval Applicability
Task Description
Thresh. Repeat APL ENG
ATA 52: Doors52.80.FC1 F NOTE 17200
FC
4000
FC
ALL ALL NTERNAL - SPECIAL DETAILED: Main Cargo Door Frames.
Inspect the outer chords of the door frames for crack-ing at all fasteners using method 1 as stated in Table 2 (see page 3) of report Aeronautical Engineers, Inc. (AEI) SIE -367-601.
ACCESS NOTE: Door secured in the closed position. Remove cargo compartment lining and gain access through the inner skin lightening holes.
52.80.FC2 (1)
F NOTE 16500
FC
6800
FC
ALL ALL EXTERNAL - SPECIAL DETAILED: Main Cargo Door Latches.
Inspect the steel latch hooks at the contact surface for cracking using method 1 as stated in Table 2 (see page 3) of report Aeronautical Engineers, Inc. (AEI) SIE -367-601.
ACCESS NOTE: Door secured in the opened position (reference the maintenance manual for this procedure).
52.80.FC2 (2)
F NOTE 5000
FC
3200
FC
ALL ALL EXTERNAL - SPECIAL DETAILED: Main Cargo Door Latches.
Inspect the bore of both lugs on each latch hook for cracking using method 2 as stated in Table 2 (see page 3) of report Aeronautical Engineers, Inc. (AEI) SIE -367-601 once the bolts have been removed.
ACCESS NOTE: Door secured in the opened position (reference the maintenance manual for this procedure).
52.80.FC3 F NOTE 5000
FC
3200
FC
ALL ALL EXTERNAL - SPECIAL DETAILED: Main Cargo Door Latch Base Lug.
Inspect the bore of the steel latch base lugs for crack-ing using method 2 as stated in Table 2 (see page 3) of report Aeronautical Engineers, Inc. (AEI) SIE -367-601 once the latch hook bolts have been removed.
ACCESS NOTE: Door secured in the opened position (reference the maintenance manual for this procedure).
Rev 0 19 March 2014
12-23
MD-80 MAINTENANCE MANUAL
52.80.FC4 F NOTE 15900
FC
7500
FC
ALL ALL INTERNAL - SPECIAL DETAILED: Main Cargo Door Frame Steel Angle at Latch Base.
Inspect the lower cargo door steel angles where the latch bases are attached for cracking around all six fas-tener holes at each location once the bolts have been removed using method 2 as stated in Table 2 (see page 3) of report Aeronautical Engineers, Inc. (AEI) SIE -367-601.
ACCESS NOTE: Door secured in the closed position. Remove cargo compartment lining and gain access through the inner skin lightening holes.
PSE
Item
Number
P
G
M
Access
Interval Applicability
Task Description
Thresh. Repeat APL ENG
52.80.FC5 F NOTE 20000
FC
15700 FC
ALL ALL INTERNAL - SPECIAL DETAILED: Main Cargo Door Frame Web at Steel Angle Attachments.
Inspect the entire lower web of the aluminum door frames and entire steel angle for cracking around all fasteners using method 1 as stated in Table 2 (see page 3) of report Aeronautical Engineers, Inc. (AEI) SIE -367-601.
ACCESS NOTE: Door secured in the closed position. Remove cargo compartment lining and gain access through the inner skin lightening holes.
52.80.FC6 F NOTE 10700
FC
3400
FC
ALL ALL EXTERNAL - SPECIAL DETAILED: Hinge Attach-ment to Main Cargo Door Skin.
Inspect all layers underneath the steel and aluminum cargo door hinge sections for cracking at all fastener holes using method 2 as stated in Table 2 (see page 3) of report Aeronautical Engineers, Inc. (AEI) SIE -367-601, once the fasteners have been removed. Complete this inspection one hinge section at a time.
ACCESS NOTE: Door secured in the closed position.
ATA 53: FUSELAGE
53.80.FC1 F NOTE 10700
FC
3400
FC
ALL ALL EXTERNAL - SPECIAL DETAILED: Hinge Attach-ment to Fuselage Skin/Surround Doubler Inspect all layers underneath the steel and aluminum fuselage hinge sections for cracking at all fastener holes using method 2 as stated in Table 2 (see page 3) of report Aeronautical Engineers, Inc. (AEI) SIE -367-601, once the fasteners have been removed. Complete this inspection one hinge section at a time.
ACCESS NOTE: Door secured in the closed position.
53.80.FC2 F NOTE 17300
FC
8000
FC
ALL ALL EXTERNAL - SPECIAL DETAILED: Surround Skin and Doubler at Cutout Corners.
Inspect surround skin and doubler at the four cutout corners for cracking at all fastener holes using method 2 as stated in Table 2 (see page 3) of report Aeronauti-cal Engineers, Inc. (AEI) SIE -367-601, once the fas-teners have been removed. Also complete an edgewise inspection of all layers using method 3.
Rev 0 19 March 2014
12-24
MD-80 MAINTENANCE MANUAL
53.80.FC3 F NOTE 20000
FC
16800 FC
ALL ALL EXTERNAL - SPECIAL DETAILED: Upper and Lower Skin Lap Splices.
Inspect new and existing skins externally and existing doublers and triplers internally for cracking at all accessible fasteners using method 1 as stated in Table 2 (see page 3) of report Aeronautical Engineers, Inc. (AEI) SIE-367-601.
ACCESS NOTE: Remove cargo compartment lining for internal inspection.
PSE
Item
Number
P
G
M
Access
Interval Applicability
Task Description
Thresh. Repeat APL ENG
53.80.FC4 F NOTE 20000FC
12500FC
ALL ALL EXTERNAL - SPECIAL DETAILED: Forward Skin Edge Butt Splice.Inspect new and existing skins externally and doubler and tripler internally for cracking at all accessible fas-teners using method 1 as stated in Table 2 (see page 3). of report Aeronautical Engineers, Inc. (AEI) SIE -367-601.ACCESS NOTE: Remove cargo compartment lining for internal inspection.
53.80.FC5 F NOTE 20000FC
10100FC
ALL ALL EXTERNAL - SPECIAL DETAILED: Aft Skin Edge Butt Splice.Inspect new skin externally and existing doubler and tri-pler internally on the forward side of the splice for cracking at all accessible fasteners using method 1 as stated in Table 2 (see page 3) of report Aeronautical Engineers, Inc. (AEI) SIE -367-601. The aft side of the butt splice is covered by PSE 53.80.004.ACCESS NOTE: Remove cargo compartment lining for internal inspection.
53.80.FC6 F NOTE 20000FC
20000FC
ALL ALL EXTERNAL - SPECIAL DETAILED: Upper Skin Butt Splice.Inspect new skin externally and spice doubler and tripler internally for cracking at all accessible splice fasteners between S-1 to S-4L using method 1 as stated in Table 2 (see page 3) of report Aeronautical Engineers, Inc. (AEI) SIE -367-601.ACCESS NOTE: Remove cargo compartment lining for internal inspection.
53.80.FC7 F 20000FC
12600FC
ALL ALL EXTERNAL - SPECIAL DETAILED: Upper Surround Doubler Butt Splice.Inspect new skin for cracking at all surround doubler splice fasteners using method 4 as stated in Table 2 (see page 3) through the t = 0.08 inch surround doubler.
Rev 0 19 March 2014
12-25
MD-80 MAINTENANCE MANUAL
53.80.FC8 F 20000FC
10500FC
ALL ALL INTERNAL - SPECIAL DETAILED: Surround Dou-bler Edge Attachments.Inspect new skin for cracking at all accessible corner surround doubler edge attachments using method 1 as stated in Table 2 (see page 3).ACCESS NOTE: Remove cargo compartment lining.
53.80.FC9 F 20000FC
6100FC
ALL ALL EXTERNAL - SPECIAL DETAILED: Lower Surround Doubler Butt Splice.Inspect new skin for cracking at all surround doubler splice fasteners using method 4 as stated in Table 2 (see page 3) through the t = 0.08 inch surround doubler.
53.80.FC10 F 20000FC
20000FC
ALL ALL EXTERNAL - SPECIAL DETAILED: Wing Scanning Light Cutout in Skin.Inspect the skin for cracking at all twelve lens assembly attachment holes using method 2 as stated in Table 2 (see page 3) once the bolts and the lens assembly have been removed.
PSE
Item
Number
P
G
M
Access
Interval Applicability
Task Description
Thresh. Repeat APL ENG
53.80.FC11 F NOTE 20000
FC
6900
FC
ALL ALL EXTERNAL - SPECIAL DETAILED: Upper Skin Patch Doubler Edges.
Inspect new and existing skins for cracking at all finger doubler attachments using method 1 as stated in Table 2 (see page 3).
53.80.FC12 F NOTE 20000
FC
20000 FC
ALL ALL EXTERNAL - SPECIAL DETAILED: GPS Antenna Doubler Installation.
Inspect skin for cracking at all internal doubler attachments and large antenna holes using method 1 as stated in Table 2 (see page 3).
ACCESS NOTE: Remove GPS antenna. No other access required for external inspection.
53.80.FC13 F NOTE 20000
FC
7500
FC
ALL ALL INTERNAL - SPECIAL DETAILED: Forward and Aft Jambs Outer Chords.
Inspect outer chords of the forward and aft jamb frames for cracking at all skin attachments between the header beam and lower sill using method 1 as stated in Table 2 (see page 3).
ACCESS NOTE: Remove cargo compartment lining and access through inner skin lightening holes.
53.80.FC14 F NOTE 20000
FC
7100
FC
ALL ALL INTERNAL - SPECIAL DETAILED: Forward and Aft Jambs Frames and Upper Bathtub Fittings.
Inspect the frame webs and bathtub splice fittings for cracking around all attachments (in the frames and fitting) using method 1 as stated in Table 2 (see page 3).
ACCESS NOTE: Remove cargo compartment lining and corner closeouts and access through inner skin lightening holes.
Rev 0 19 March 2014
12-26
MD-80 MAINTENANCE MANUAL
53.80.FC15 F 10300
FC
4200
FC
ALL ALL INTERNAL - SPECIAL DETAILED: Forward and Aft Jambs Frames and Lower Bathtub Fit-tings.
Inspect the frame webs and bathtub splice fittings for cracking around all attachments (in the frames and fitting) using method 1 as stated in Table 2 (see page 3).
ACCESS NOTE: Remove cargo compartment lining and corner closeouts and access through inner skin lightening holes.
53.80.FC16 F 20000
FC
20000 FC
ALL ALL EXTERNAL - SPECIAL DETAILED: Header Beam Outer Chord.
Inspect the header beam outer chord for cracking at all six hinge plate/extension plate splice plate holes (hinge plate is steel and extension plate, splice plate, and header beam are aluminum) using method 2 as stated in Table 2 (see page 3) once the fasteners have been removed. It is acceptable to first oversize the hi-lok fasteners attaching the hinge plates to the splice joint.
PSE
Item
Number
P
G
M
Access
Interval Applicability
Task Description
Thresh. Repeat APL ENG
53.80.FC17 F NOTE 20000
FC
18500
FC
ALL ALL INTERNAL - SPECIAL DETAILED: Header Beam Inner Chord.
Inspect the header beam inner chord for cracking around the inner strap attachments from the edge of the strap to the nearest frame station using method 1 as stated in Table 2 (see page 3).
ACCESS NOTE: Remove cargo compartment lining and access through inner skin lightening holes.
53.80.FC18 F NOTE 20000
FC
20000
FC
ALL ALL INTERNAL - SPECIAL DETAILED: Header Beam Inner Chord Angle.
Inspect the header beam inner chord angle for cracking around the last five rows of inner strap attachments and the four gusset plate attachments at each end of the header beam using method 1 as stated in Table 2 (see page 3).
ACCESS NOTE: Remove cargo compartment lining and access through inner skin lightening holes.
53.80.FC19 F NOTE 20000
FC
20000
FC
ALL ALL INTERNAL/EXTERNAL - SPECIAL DETAILED: Header Beam Web Cutouts.
Externally inspect the extension plate at four fasteners on either side of the header beam web cutouts for cracking around the attachments using method 1 as stated in Table 2 (see page 3). Internally inspect the header beam for a completely failed chord using a detailed visual inspection.
ACCESS NOTE: None required for the external inspec-tion. Remove cargo compartment lining and corner close-outs and access through inner skin lightening holes for the internal inspection.
Rev 0 19 March 2014
12-27
MD-80 MAINTENANCE MANUAL
53.80.FC20 F 20000
FC
2800
FC
ALL ALL EXTERNAL - SPECIAL DETAILED: Skin at Forward Header Beam Runout.
Inspect the skin along both edges of the extension plate between FS370 to FS389 for cracking emanating out from underneath the extension plate edges using method 1 as stated in Table 2 (see page 3).
53.80.FC21 F 20000
FC
5600
FC
ALL ALL EXTERNAL - SPECIAL DETAILED: Skin at Aft Header Beam Runout Shim.
Attachments.
Inspect the skin along both edges of the shim between FS541 to FS560 for cracking emanating out from under-neath the shim edges using method 1 as stated in Table 2 (see page 3).
53.80.FC22 F NOTE 14500
FC
4000
FC
ALL ALL INTERNAL - SPECIAL DETAILED: Skin at Aft Header Beam Stringer.
Runout.
Inspect the skin along both edges of the stringer cap for cracking emanating out from underneath the cap edges using method 1 as stated in Table 2 (see page 3).
ACCESS NOTE: Remove cargo compartment lining.
PSE
Item
Number
P
G
M
Access
Interval Applicability
Task Description
Thresh. Repeat APL ENG
53.80.FC23 F 15700
FC
5800
FC
ALL ALL EXTERNAL - SPECIAL DETAILED: Shim at Aft Header Beam Stringer.
Runout.
Inspect the shim at the last two rows of stringer runout attachments for cracking around the fasteners using method 1 as stated in Table 2 (see page 3).
53.80.FC24 F 6700
FC
4200
FC
ALL ALL EXTERNAL - SPECIAL DETAILED: Skin and Shim at Aft Extension Plate.
Runout.
Inspect the skin and shim at the last row of extension plate attachments for cracking around the fastener holes using method 2 as stated in Table 2 (see page 3) once the fasten-ers have been removed. It is acceptable to first oversize these three hi-lok fasteners.
53.80.FC25 F NOTE 20000
FC
4200
FC
ALL ALL INTERNAL - SPECIAL DETAILED: Upper Stub Frame Inner Chords.
Inspect the inner cap of all stub frames between the header beam and S-3R (or S-2L) for cracking around any fasten-ers using method 1 as stated in Table 2 (see page 3).
ACCESS NOTE: Remove cargo compartment lining and access through inner skin lightening holes where neces-sary.
Rev 0 19 March 2014
12-28
MD-80 MAINTENANCE MANUAL
53.80.FC26 F NOTE 10300
FC
4400
FC
ALL ALL EXTERNAL - SPECIAL DETAILED: Latch Plate Lugs.
Inspect the steel latch plate lugs for cracking at the lug hole once the spool bolt has been removed using method 2 as stated in Table 2 (see page 3).
ACCESS NOTE: Door secured in the opened position (reference the maintenance manual for this procedure).
53.80.FC27 F NOTE 16700
FC
6000
FC
ALL ALL INTERNAL - SPECIAL DETAILED: Lower Frame at Latch Plate.
Attachments.
Inspect the lower frame webs for cracking around the last row of the latch plate attachments (two latch plates per frame station listed) using method 1 as stated in Table 2 (see page 3).
ACCESS NOTE: Remove cargo compartment lining.
53.80.FC28 F NOTE 20000
FC
13300
FC
ALL ALL INTERNAL - SPECIAL DETAILED: Latch Plate at Lower Frame.
Attachments.
Inspect the steel latch plates at the first row of lower frame attachments for cracking at the fastener hole using method 2 as stated in Table 2 (see page 3) once the two bolts going through the spacer block at each location have been removed.
ACCESS NOTE: Remove cargo compartment lining.
PSE
Item
Number
P
G
M
Access
Interval Applicability
Task Description
Thresh. Repeat APL ENG
53.80.FC29 F NOTE 8100
FC
3100
FC
ALL ALL INTERNAL - SPECIAL DETAILED: Lower Sill Web Cutouts at Forward/Aft.
Jambs.
Inspect the lower sill web on both the upper and lower sur-faces at the forward and aft jamb stations FS389, FS397, FS533, and FS541 for cracking at the web cutouts using method 1 as stated in Table 2 (see page 3).
ACCESS NOTE: Remove cargo compartment lining and corner closeouts and access through inner skin lightening holes where necessary.
53.80.FC30 F NOTE 20000
FC
6800
FC
ALL ALL EXTERNAL - SPECIAL DETAILED: Lower Sill Web Cutouts at Latch Spools.
Inspect the lower sill web on the upper surface at all seven latch spool locations for cracking at the web cutouts using method 1 as stated in Table 2 (see page 3).
ACCESS NOTE: Door secured in the opened position (reference the maintenance manual for this procedure).
Rev 0 19 March 2014
12-29
MD-80 MAINTENANCE MANUAL
53.80.FC31 F NOTE 19800
FC
6500
FC
ALL ALL INTERNAL - SPECIAL DETAILED: Existing Lower Frame Splice.
Inspect the existing frame, new frame, angle, and splice at FS389 and FS541 between stringers S-24L and S-26L for cracking around all splice attachments using method 1 as stated in Table 2 (see page 3).
ACCESS NOTE: Remove cargo compartment lining.
53.80.FC32 F NOTE 20000
FC
8700
FC
ALL ALL INTERNAL - SPECIAL DETAILED: Lower Stub Frame Inner Chords.
Inspect the stub frame inner chords from FS389 to FS541 between the lower sill and S-23L for cracking around all inner chord fastener holes using method 1 as stated in Table 2 (see page 3).
ACCESS NOTE: Remove cargo compartment lining.
53.80.FC33 F 20000
FC
5400
FC
ALL ALL EXTERNAL - SPECIAL DETAILED: Existing Stringer Forward Runouts.
Inspect the existing stringer for cracking around all runout attachments using method 4 as stated in Table 2 (see page 3) through either the existing skin or new skin from string-ers S-1 to S-6L.
53.80.FC34 F NOTE 20000
FC
9700
FC
ALL ALL INTERNAL - SPECIAL DETAILED: Existing Stringer Aft Runouts.
Inspect the existing stringer for cracking around all runout attachments using method 4 as stated in Table 2 (see page 3) through the splice fitting from stringers S-1 to S-5L.
ACCESS NOTE: Remove cargo compartment lining.
PSE
Item
Number
P
G
M
Access
Interval Applicability
Task Description
Thresh. Repeat APL ENG
53.80.FC35
F NOTE 2600
FC
1000
FC
ALL ALL INTERNAL - SPECIAL DETAILED: Existing Floor Beam at Frame Fitting in MCD Cutout Area.
Inspect the existing floor beam web for cracking around all fitting attachments using method 1 as stated in Table 2 (see page 3) at stations FS408-522.
ACCESS NOTE: Remove cargo compartment lining and floor panels or gain access from the lower lobe after the cargo liner has been removed.
Rev 0 19 March 2014
12-30
MD-80 MAINTENANCE MANUAL
53.80.FC36
F NOTE 2100
FC
1100
FC
ALL ALL INTERNAL - SPECIAL DETAILED: Existing Frame at Floor Fitting in MCD.
Cutout Area.
Inspect the existing frame web at the floor fitting joint for a completely failed web using a detailed visual inspection at stations FS408-522.
ACCESS NOTE: Remove cargo compartment lining and floor panels or gain access from the lower lobe after the cargo liner has been removed.
53.80.FC37
F NOTE 19000
FC
7400
FC
ALL ALL INTERNAL - SPECIAL DETAILED: Fitting at Floor Beam to Frame Joint in MCD Cutout Area.
Inspect the fitting minimum cross-cross-section at the floor beam to frame joint for cracking using method 1 as stated in Table 2 (see page 3) at stations FS408-522.
ACCESS NOTE: Remove cargo compartment lining and floor panels or gain access from the lower lobe after the cargo liner has been removed.
53.80.FC38
F NOTE 20000
FC
9600
FC
ALL ALL INTERNAL - SPECIAL DETAILED: Existing Floor Beam at Fwd and Aft.
Jamb Frame Fittings.
Inspect the existing floor beam web for cracking around all fitting attachments using method 1 as stated in Table 2 (see page 3) at stations FS389 and 541.
ACCESS NOTE: Remove cargo compartment lining and floor panels or gain access from the lower lobe after the cargo liner has been removed.
53.80.FC39
F NOTE 20000
FC
20000
FC
ALL ALL INTERNAL - SPECIAL DETAILED: Lower Fwd and Aft Jamb Frames at Floor Beam Fittings.
Inspect the lower jamb frame webs for cracking around all floor beam fitting attachments using method 1 as stated in Table 2(see page 3) at stations FS389 and 541.
ACCESS NOTE: Remove cargo compartment lining and floor panels or gain access from the lower lobe after the cargo liner has been removed.
PSE
Item
Number
P
G
M
Access
Interval Applicability
Task Description
Thresh. Repeat APL ENG
53.80.003 F 49237
FC
3900
FC
ALL ALL INTERNAL - SPECIAL DETAILED: Fuselage Skin Panels from Longeron 3L to 3R.
See Document L26-022 PSE 53.80.003 for access and specific inspection instructions.
Rev 0 19 March 2014
12-31
MD-80 MAINTENANCE MANUAL
53.80.004 F 63725
FC
7300
FC
ALL ALL INTERNAL - SPECIAL DETAILED: Fuselage Skin Splices from Longeron 5L to 5R.
These new inspection intervals only apply to the exist-ing skin on the forward side of FS588 between S-1 to S-5R and the aft side between S-5L to S-5R and both sides of FS759 between S-5L to S-5R. See Document L26-022 PSE 53.80.004 for access and specific inspec-tion instructions.
53.80.006 F 66946
FC
8800
FC
ALL ALL INTERNAL - SPECIAL DETAILED: Fuselage Frame to Floor Beam Joints.
Over Main Landing Gear, FS946, FS965, FS984 See Document L26-022 PSE 53.80.006 for access and spe-cific inspection instructions.
53.80.016 F 71376
FC
33300
FC
ALL ALL INTERNAL - SPECIAL DETAILED: Fuselage Skin and Frames from Longeron 15 to 18, FS1041, FS1060, FS1079, FS1098.
See Document L26-022 PSE 53.80.016 for access and specific inspection instructions.
53.80.017 F 1C 1C ALL ALL INTERNAL - SPECIAL DETAILED: Longerons 16 and 17 Above Forward Lower Cargo Door Jamb.
This existing PSE is in the area directly across form the main cargo door cutout. There is potential for runaway pallets slamming into the fuselage structure being inspected so the new reduced inspection intervals are every C Check since modification.
See Document L26- 022 PSE 53.80.017 for access and specific inspection instructions.
53.80.019 F 51662
FC
2350
FC
ALL ALL INTERNAL - SPECIAL DETAILED: Forward Lower Cargo Door Jamb Corners.
See Document L26-022 PSE 53.80.019 for access and specific inspection instructions.
Rev 0 19 March 2014
12-32
MD-80 MAINTENANCE MANUAL
12.5 Inspection Instructions for VAI 9G Barrier Installation, DC-9-80 and MD-88 Aircraft
1. General.
Prior to accumulating the total number of cycles on the aircraft at which the threshold inspection should be initiated, and thereafter at the associated repeat intervals shown in this document, perform the following high frequency eddy current (ETHF) inspections to insure no cracks are detectable in the affected aircraft structure.
NOTE: The inspections should verify that there are no cracks in the affected aircraft structure. If cracks are detected they must be repaired prior to further flight.
Figure 12-G: Douglas NDTSPM, MDC93K0393, Part 06 Inspection MethodsReference Table
Figure 12-H: VAI 9G Barrier Installation Inspection Tasks
Perform an internal high frequency eddy current (ETHF) inspection using method 1 as called out in Table 1 at a threshold of 20,000 flights (landings) since installation of the 9G barrier as follows. At stringers S-1, S-9R, S-16R, S-17R, S-16L, and S-17L, inspect the stringer caps along the edges of the filler for the length of the four fasteners forward of station 237 as shown in the figures in SIE-367-602.
At stringers S-2R to S-8R, S-10R, and S-2L to S-10L, inspect the stringer caps around the fastener heads of the six fasteners attaching the straps aft of station 237 and inspect the stringer caps along the edges of the filler for the length of the four fasteners forward of station 237 as shown in the the figures in SIE-367-602.
At stringers S-11R and S-11L, inspect the stringer caps around the fastener heads of the six fasteners attaching the straps aft of station 237 and inspect the stringer caps along the edges of the filler or flexure for the length of the eight fasteners forward of station 237 as shown in the figures in SIE-367-602.
At stringers S-15R and S-15L, inspect the stringer caps along the edges of the filler or flexure for the length of the eight fasteners forward of station 237 as shown in the figures in SIE-367-602.
Repeat this ETHF inspection of the stringers thereafter at repeat intervals not to exceed 20,000 flights (landings).
Method Inspection Section Subject No.
1 ETHF surface and filled holes 10 01 001
MPD
Item
No.
Task Interval Zone Access
Applicability
Man-
Hours
Task Description
APL ENG
ATA 53: 9G Bulkhead Stringer Attach-ment
53-TNK-01-01 SDI 20,000
FC
51 NOTE ALL ALL 2.0 Comply with inspection requirements in the following references:
Structural Integrity Engineering (SEI) 367-602 latest revision.
Douglas NDTSPM MDC93K0393, Part 06 Inspection Methods Reference Table.
Rev 0 19 March 2014
12-33
MD-80 MAINTENANCE MANUAL
12.6 Cargo Loading System
1. Scope.
The purpose of these items are to provide Instructions for Continued Airworthiness (ICA) in accordance with 14 CFR 25.1529 for the ANCRA cargo loading system as installed on the MD-80SF.
2. Applicability.
These items are applicable to the MD-80SF with ANCRA Main Deck Cargo Loading System Part number 85130 series installed. For all other aircraft components refer to their applicable Instruction for Continued Airworthiness (ICA) documents.
3. Distribution of Instructions for Continued Airworthiness.
The original ICA was distributed and delivered to Aeronautical Engineering Inc., the STC holder by ANCRA prior to delivery of the aircraft to the Everts Air Cargo.
Future FAA approved revisions of the ICA will be delivered to Aeronautical Engineering Inc. for distribu-tion to Everts.
4. Units of Measure.
Length - Inches.
Weight - Pounds.
5. Reference.
• Aircraft Weight and Balance Control Manual.
• CMM/IPL 25-51-67 Rev N/C dated 1/1/12.
• NAS 3610 Revision 10, dated November 1990.
• SAE AS 36100 Revision A, dated 4/27/2006 (CMM 25-50-00).
12.6.1 General Description of Cargo Loading System
The ANCRA 85130 Series MDCLS installed on the MD-80 aircraft, designed to accommodate standard ULDs. The ULDs allowed to be used and loaded in this cargo loading system must comply with the requirements of AS 36100 or NAS3610.
All MDCLS components are installed using quick release or permanent fasteners and are attached to the aircraft seat tracks.
12.6.2 MDCLS Functionality and Subcomponents
The MDCLS is designed to provide conveyance and guidance for ULD as well as restraint devices to sup-port the imposed flight loads.
1. The MDCLS consists of the following major components:
a. Conveyance system.
• Roller trays.
• Ballmats.
• Doorsill protector.
b. Guidance.
• Continuous side guide rails all around the system.
c. Restraint System.
• XZ restraint devices providing Forward/Aft and Vertical restraint.
Rev 0 19 March 2014
12-34
MD-80 MAINTENANCE MANUAL
• YZ restraint system retractable providing Inboard/Outboard and Vertical restraint.
12.6.3 Airworthiness Limitations
The Airworthiness Limitations section in ANCRA report 9682, is FAA-approved and specifies mainte-nance required under §43.16 and §91.403 of the Federal Aviation Regulations, unless an alternative pro-gram has been FAA approved.
No other Airworthiness Limitation is associated with this STC.
12.6.4 Placards
Loading placards indicating authorized loading configurations/maximum positional weight is installed on the sidewall lining of the aircraft. The maximum ULD weight cannot exceed the maximum weight indi-cated on the placard. For aircraft loading instructions and limitation see aircraft W&B manual.
12.6.5 Cleaning
Refer to ANCRA CMM/IPL 25-51-67, Cleaning Section, for MDCLS cleaning procedures.
12.6.6 Inspections
1. Preloading Inspection at Each Loading Cycle.
Doorsill Protector:
• Make sure the doorsill protector is operative and can be lowered and stowed properly. Inspect all equipment on the doorsill such as rollers and side guides for proper functionality (verify by operat-ing the equipment).
Walkthrough and visual inspection.
The purpose of this inspection is to identify obvious missing or broken LRUs to ensure loading is safe and complies with intended function of the cargo system.
• Before loading, walk through the main deck and inspect that all locks are installed. Inspect that the end stops are installed.
• Inspect all side guides to ensure that they are not damaged to result in ULD getting jammed.
Inspect that the ball mat surface is clean and if any ball units are missing. Inspect the roller conveyance system for missing or broken rollers. Although missing rollers and ball units do not constitute missing restraint condition, but large area without roller/ball support impact the functionality of the cargo system and increase the system rolling friction due to ULD sagging. Therefore following loading limitation shall apply:
• ULD cannot be parked and locked in a position where more than 10% of the ball units are missing in this area.
• ULD cannot be parked and locked in a position where more than 10% of the rollers are missing in this area.
Make sure MDCLS is free from foreign objects. Remove cord, plastic wrap, ice, liquid, animal waste, and trash from around components. Remove any liquid that has flowed around components. This is important to prevent corrosion.
Inspect aircraft floor and seat tracks for loose fasteners, if loose fasteners are found, check if they belong to the cargo equipment. If the fastener belongs to cargo equipment, consult CMM/IPL 25-51-67 to repair or replace the damaged component.
Rev 0 19 March 2014
12-35
MD-80 MAINTENANCE MANUAL
Missing or Broken Restraint.
• If any of the restraint devices is damaged (missing or broken), ULD weight at that position is either reduced or the position must be void. Refer to W&B for disposition. In case of any doubt or lack of information, a position with broken or missing restraint MUST stay void.
2. Component Operational Check.
Refer to ANCRA CMM/IPL 25-51-67 Check Section for Component Operational Check.
3. Overhaul Inspection and Maintenance Schedule.
To better protect and preserve the cargo system components, a scheduled removal for the entire system is planned every 28,800 flight hours or 120 month, whichever comes first. Entire MDCLS is removed to gain access to the floor structure for heavy maintenance. At this opportunity the MDCLS must be completely inspected and overhauled to remove corroded parts and parts with excessive wear and tear or any other damages. Refer to ANCRA CMM/IPL 25-51-67 Check Section for MDCLS Overhaul Inspection and Maintenance Schedule.
4. System Operational Check.
System Operational Check is necessary when major part or the entire cargo loading system is removed from the aircraft and is reinstalled. Using the System Operational Check the installer can verify that the system is installed correctly (parts in right place). Refer to ANCRA CMM/IPL 25-51-67 Check Section for MDCLS Operational Check.
5. Servicing and Lubrication.
The MDCLS does not require scheduled servicing and lubrication.
6. Degree of Inspection.
All inspections for LRUs installed on aircraft are only visual. Components before and after repair require an operational check as outlined in CMM/IPC 25-51-67.
7. Troubleshooting.
The following simple procedure applies when a local malfunction is identified:
a. If a component (LRU) does not function properly, the LRU must be replaced, there is no quick fix.
b. If a ULD is jammed, check the reason for jamming, it is usually the nets have caught on the restraint or under pallet or an object is protruding outside the envelop of the ULD, remove the obstacle to free ULD. Do not use a pry bar.
c. Utilize loading aid and guidance devices provided to safely operate the cargo loading system. Refer to aircraft owner/operator documentation.
12.6.7 Applicable Wear Tolerances
As a result of aircraft movement as well as loading and unloading of ULDs, the surfaces of the cargo com-ponents in contact with the ULDs are subjected to wear. Wear on cargo components can be observed in the following areas.
Components Wear Limits Disposition
Door sill protector. Replace when no longer functional. Not structural parts, operator disposition.
Roller trays and rollers. Replace when no longer functional. Not structural parts, operator disposition.
Ball mats Replace when no longer functional. Not structural parts, operator disposition.
Side guide rail. Replace when no longer functional. Not structural parts, operator disposition.
Rev 0 19 March 2014
12-36
MD-80 MAINTENANCE MANUAL
12.6.8 Corrosion
The MDCLS is subjected to water from wet ULDs or liquid deposited from freight. Components have ade-quate corrosion protection when delivered from the factory.
However due to normal wear and tear and exposure to corrosive agents the cargo component may be sub-ject to corrosion. To avoid corrosion to the cargo components it is recommended that they be cleaned with water and air-dried periodically. Minor surface corrosion and pigments on the Cargo components are com-mon, but if the corrosion is any more than minor surface corrosion and pigments the LRU must be removed and restored per CMM/IPC. No standard rework procedure to salvage the corroded cargo compo-nents is available due to complexity of the assemblies.
1. Corrosion Prevention.
a. See Section 7.3 for maintenance schedule.
12.6.9 Component Removal and Installation
Majority of cargo components use studs and standard nuts for installation in the seat track. Use standard mechanic tools to remove the component from the seat track. Refer to CMM/IPL 25-51-67 “Description and Operation” Section for removal and installation of ANCRA components.
12.6.10 Torque Requirements
All fasteners used in the MDCLS are MS, NAS, or AN standard. There is no need to remove and replace the hardware at any time during the life of the aircraft unless the LRU is damaged. Refer to instructions provided in CMM/IPL 25-51-67 for hardware replacement during repair and overhaul as well as the appli-cable torque value for each fastener.
12.6.11 Storage Instructions
The MDCLS components must be stored in an indoor warehouse. Some rollers contain sealed ball bearings and it is recommended storing them in a horizontal shelving system. Storing these rollers in vertical posi-tion will drain the grease from the ball bearings, impacting the performance of the roller.
12.6.12 Lubrication
No lubrication is needed for the cargo equipment.
12.6.13 EWIS Impact
Installation of the MDCLS on the aircraft has been evaluated per guidance provided in FAA AC 25-27A. It has been determined that the MDCLS has no electrical components, does not penetrate the floor or side-walls, and does not affect the airplane electrical wiring interconnection system (EWIS) through introduc-tion of structure, potential interference or contact, or pathways for foreign objects. The 85130 series MDCLS does not necessitate preparation of an EWIS ICA, nor revision to the previously approved EWIS ICA, that would be required to be developed under 14CFR 26.11(b).\
Cargo locks, end stops, doorway restraints, and crosstracks.
At the contact surface with ULD wear and scratch not exceeding .060” depth.
Refer to Aircraft W&B.
Rev 0 19 March 2014
12-37
MD-80 MAINTENANCE MANUAL
Figure 12-I: ANCRA MD-80 Cargo Loading System Tasks
12.7 ARTEX C406-1 Emergency Locator Transmitter (ELT) System
1. Purpose.
This section is intended to fulfill the requirements of FAR Part 25.1529 by providing complete instructions for continued airworthiness relative to the modification and installation of an ARTEX C406-1 Emergency Locator Transmitter (ELT) System.
The report and the instructions contained herein supplement instructions included in the OEM manuals. Instructions contained in EMTEQ report 2-22566-905 will supersede or modify instructions contained in OEM manuals only where specifically stated in that report.
If any question arises from conflicting or contradictory instructions contained in any manuals, EMTEQ Engineering should be consulted before commencing to use those instructions.
MPD
Item
No.
Task Interval Zone Access
Applicability
Man-
Hours
Task Description
APL ENG
ATA 25: Equipment / Furnishings
25-TNK-02-01 10 YR
10 YR / 28,000
FC
51 NOTE ALL ALL 200 Detailed Inspection of the ANCRA cargo loading system per CMM 25-51-67.
INTERVAL NOTE: Whichever comes first.
ACCESS NOTE: With all system com-ponents removed.
25-TNK-02-02 INS 125
FC
51 NOTE ALL ALL .1 Walkthrough and Visual Inspection:
Detailed Inspection:
Before loading, walk through the main deck and inspect that all locks are installed. Inspect that the end stops are installed.
Inspect all side guids to ensure that they are not damaged to result in ULD getting jammed.
Rev 0 19 March 2014
12-38
MD-80 MAINTENANCE MANUAL
Figure 12-J: ELT Maintenance & Inspection Tasks
12.8 ELT Installation Structural Inspection Requirements
1. Inspection Method.
The connector hole and fastener holes should be inspected to the intervals outlined in the table bellow (Ref EMTEQ document 2-22566), using the eddy current inspection procedures as specified in the EMTEQ NDT Maintenance Manual Supplement Document No. 2-120483-800 Chapters 51-EQ-03, 51-EQ-05, 51-EQ06, and 51-EQ-08. The detectable crack length for eddy current inspection techniques is 0.05”. The threshold crack length for each location indicates that a crack should be detectable at the time of the thresh-old inspection. For the connector hole, the inspector should look for cracks on the surfaces of the skin and doubler around the connector hole. For the fastener holes, the inspector should look for cracks on the sur-faces of the skin and doubler around the fastener holes. Circle templates are included to aid in inspection. The circle template that should be used for this modification is outlined in EMTEQ document 2-22566 table L-II.
2. Corrective Action.
Should a crack be detected using the inspection specified, contact EMTEQ Engineering with details (i.e. locations and crack length) for repair instructions.
MPD
Item
No.
Task Interval Zone Access
Applicability
Man-
Hours
Task Description
APL ENG
ATA 25: Equipment / Furnishings
25-TNK-01-01 1YR 1YR 51 NOTE ALL ALL 1 Perform a system inspection per EMTEQ MM Supplement 25-65-60/201 (Doc. 2-22566-915).
25-TNK-01-02 5YR 5YR 51 NOTE ALL ALL 1 Remove and replace the ELT Transmitter per the Replacement EMTEQ MM Sup-plement 25-65-90/401 (Doc. 2-22566-913). Ship ELT Transmitter to the appro-priate repair facility for battery replace-ments.
Rev 0 19 March 2014
12-39
MD-80 MAINTENANCE MANUAL
Figure 12-K: Structural Inspection Requirements Tasks
MPD
Item
No.
Task Interval Zone Access
Applicability
Man-
Hours
Task Description
APL ENG
ATA 53: Fuselage
53-TNK-02-01 SDI 72,079
FC
59 NOTE ALL ALL .5 INTERNAL - SPECIAL DETAILED: Connector Hole - Inspect ELT connec-tor hole for cracks.
Do a high frequency eddy current inspection of the ELT antenna connec-tor hole for cracks.
ACCESS NOTE: Remove cargo compartment lining.
NOTE: Procedure can be found in EMTEQ Doc. 2-22566-905, para-graph 15.1.2.
53-TNK-02-02 SDI 20,043
FC
59 NOTE ALL ALL .5 INTERNAL - SPECIAL DETAILED: Fastener Holes - Inspect ELT fastener holes for cracks.
Do a high frequency eddy current inspection of the ELT antenna fastener holes for cracks.
ACCESS NOTE: Remove cargo compartment lining.
NOTE: Procedure can be found in EMTEQ Doc. 2-22566-905.
Rev 0 19 March 2014
12-40
MD-80 MAINTENANCE MANUAL
Intentionally Left Blank
Rev 0 19 March 2014
Appendix A LEP-1
List of Effective Pages - Appendix A
Ch. # Page # Card # Ch. # Page # Card #
MD-80 MAINTENANCE MANUAL
Appendix A 1 25-TNK-01-01Appendix A 2 25-TNK-01-01Appendix A 3 25-TNK-01-02Appendix A 4 25-TNK-01-02Appendix A 5 25-TNK-02-01Appendix A 6 25-TNK-02-01Appendix A 7 25-TNK-02-02Appendix A 8 25-TNK-02-02Appendix A 9 25-TNK-02-02Appendix A 10 25-TNK-02-02Appendix A 11 AE-26-030-01-01Appendix A 12 AE-26-030-01-01Appendix A 13 AE-29-050-01-01Appendix A 14 AE-29-050-01-01Appendix A 15 AE-29-050-02-01Appendix A 16 AE-29-050-02-01Appendix A 17 AE-29-050-02-01Appendix A 18 AE-29-050-02-01Appendix A 19 AE-29-050-03-01Appendix A 20 AE-29-050-03-01Appendix A 21 AE-29-050-03-01Appendix A 22 AE-29-050-03-01Appendix A 23 AE-29-050-04-01Appendix A 24 AE-29-050-04-01Appendix A 25 AE-29-050-04-01Appendix A 26 AE-29-050-04-01Appendix A 27 AE-29-050-05-01Appendix A 28 AE-29-050-05-01Appendix A 29 AE-29-050-05-01Appendix A 30 AE-29-050-05-01Appendix A 31 AE-29-050-06-01Appendix A 32 AE-29-050-06-01Appendix A 33 AE-29-050-06-01Appendix A 34 AE-29-050-06-01Appendix A 35 AE-29-050-07-01Appendix A 36 AE-29-050-07-01Appendix A 37 AE-29-050-07-01Appendix A 38 AE-29-050-07-01
Appendix A 39 AE-29-050-08-01Appendix A 40 AE-29-050-08-01Appendix A 41 AE-29-050-08-01Appendix A 42 AE-29-050-08-01Appendix A 43 AE-29-050-09-01Appendix A 44 AE-29-050-09-01Appendix A 45 AE-29-050-09-01Appendix A 46 AE-29-050-09-01Appendix A 47 AE-32-080-01-01Appendix A 48 AE-32-080-01-01Appendix A 49 AE-32-080-01-01Appendix A 50 AE-32-080-01-01Appendix A 51 AE-35-020-01-01Appendix A 52 AE-35-020-01-01Appendix A 53 AE-35-020-01-01Appendix A 54 AE-35-020-01-01Appendix A 55 AE-35-020-01-01Appendix A 56 AE-35-020-01-01Appendix A 57 AE-35-020-02-01Appendix A 58 AE-35-020-02-01Appendix A 59 AE-35-020-02-01Appendix A 60 AE-35-020-02-01Appendix A 61 AE-52-031-01-01Appendix A 62 AE-52-031-01-01Appendix A 63 AE-52-031-01-01Appendix A 64 AE-52-031-01-01Appendix A 65 AE-52-031-02-01Appendix A 66 AE-52-031-02-01Appendix A 67 AE-52-031-03-01Appendix A 68 AE-52-031-03-01Appendix A 69 AE-52-031-03-01Appendix A 70 AE-52-031-03-01Appendix A 71 AE-52-031-04-01Appendix A 72 AE-52-031-04-01Appendix A 73 AE-52-031-04-01Appendix A 74 AE-52-031-04-01Appendix A 75 AE-52-031-05-01Appendix A 76 AE-52-031-05-01
Rev 0 19 March 2014
Appendix A LEP-2
List of Effective Pages - Appendix A
Ch. # Page # Card # Ch. # Page # Card #
MD-80 MAINTENANCE MANUAL
Appendix A 77 AE-52-031-06-01Appendix A 78 AE-52-031-06-01Appendix A 79 AE-52-031-07-01Appendix A 80 AE-52-031-07-01Appendix A 81 AE-52-031-08-01Appendix A 82 AE-52-031-08-01Appendix A 83 AE-52-031-09-01Appendix A 84 AE-52-031-09-01Appendix A 85 AE-52-031-09-01Appendix A 86 AE-52-031-09-01Appendix A 87 AE-52-031-10-01Appendix A 88 AE-52-031-10-01Appendix A 89 AE-52-031-10-01Appendix A 90 AE-52-031-10-01Appendix A 91 AE-52-031-10-01Appendix A 92 AE-52-031-10-01Appendix A 93 AE-52-031-10-01Appendix A 94 AE-52-031-10-01Appendix A 95 AE-52-031-10-01Appendix A 96 AE-52-031-10-01Appendix A 97 AE-52-031-10-01Appendix A 98 AE-52-031-10-01Appendix A 99 AE-52-031-10-01Appendix A 100 AE-52-031-10-01Appendix A 101 AE-52-031-11-01Appendix A 102 AE-52-031-11-01Appendix A 103 AE-52-031-12-01Appendix A 104 AE-52-031-12-01Appendix A 105 AE-52-031-12-01Appendix A 106 AE-52-031-12-01Appendix A 107 AE-52-031-12-01Appendix A 108 AE-52-031-12-01Appendix A 109 AE-52-031-12-01Appendix A 110 AE-52-031-12-01Appendix A 111 AE-52-031-12-01Appendix A 112 AE-52-031-12-01Appendix A 113 AE-52-031-12-01Appendix A 114 AE-52-031-12-01
Appendix A 115 AE-52-031-12-01Appendix A 116 AE-52-031-12-01Appendix A 117 AE-52-031-12-01Appendix A 118 AE-52-031-12-01Appendix A 119 AE-52-031-12-01Appendix A 120 AE-52-031-12-01Appendix A 121 AE-52-031-12-01Appendix A 122 AE-52-031-12-01Appendix A 123 AE-52-031-12-01Appendix A 124 AE-52-031-12-01Appendix A 125 AE-52-031-12-01Appendix A 126 AE-52-031-12-01Appendix A 127 AE-52-031-12-01Appendix A 128 AE-52-031-12-01Appendix A 129 AE-52-031-12-01Appendix A 130 AE-52-031-12-01Appendix A 131 AE-52-031-13-01Appendix A 132 AE-52-031-13-01Appendix A 133 AE-52-031-13-01Appendix A 134 AE-52-031-13-01Appendix A 135 AE-52-031-14-01Appendix A 136 AE-52-031-14-01Appendix A 137 AE-52-031-14-01Appendix A 138 AE-52-031-14-01Appendix A 139 AE-52-031-15-01Appendix A 140 AE-52-031-15-01Appendix A 141 AE-52-031-15-01Appendix A 142 AE-52-031-15-01Appendix A 143 AE-52-031-16-01Appendix A 144 AE-52-031-16-01Appendix A 145 AE-52-031-16-01Appendix A 146 AE-52-031-16-01Appendix A 147 AE-52-031-17-01Appendix A 148 AE-52-031-17-01Appendix A 149 AE-52-031-17-01Appendix A 150 AE-52-031-17-01Appendix A 151 AE-52-031-18-01Appendix A 152 AE-52-031-18-01
Rev 0 19 March 2014
Appendix A LEP-3
List of Effective Pages - Appendix A
Ch. # Page # Card # Ch. # Page # Card #
MD-80 MAINTENANCE MANUAL
Appendix A 153 AE-52-031-18-01Appendix A 154 AE-52-031-18-01Appendix A 155 AE-52-031-19-01Appendix A 156 AE-52-031-19-01Appendix A 157 AE-52-031-19-01Appendix A 158 AE-52-031-19-01Appendix A 159 AE-52-031-20-01Appendix A 160 AE-52-031-20-01Appendix A 161 AE-52-031-20-01Appendix A 162 AE-52-031-20-01Appendix A 163 AE-52-031-21-01Appendix A 164 AE-52-031-21-01Appendix A 165 AE-52-031-21-01Appendix A 166 AE-52-031-21-01Appendix A 167 AE-52-031-22-01Appendix A 168 AE-52-031-22-01Appendix A 169 AE-52-071-01-01Appendix A 170 AE-52-071-01-01Appendix A 171 AE-52-071-02-01Appendix A 172 AE-52-071-02-01Appendix A 173 AE-52-071-02-01Appendix A 174 AE-52-071-02-01Appendix A 175 AE-52-071-03-01Appendix A 176 AE-52-071-03-01Appendix A 177 AE-52-071-04-01Appendix A 178 AE-52-071-04-01Appendix A 179 AE-52-071-05-01Appendix A 180 AE-52-071-05-01Appendix A 181 AE-52-071-06-01Appendix A 182 AE-52-071-06-01Appendix A 183 AE-52-071-07-01Appendix A 184 AE-52-071-07-01Appendix A 185 AE-52-071-08-01Appendix A 186 AE-52-071-08-01Appendix A 187 AE-52-071-09-01Appendix A 188 AE-52-071-09-01Appendix A 189 AE-52-071-09-01Appendix A 190 AE-52-071-09-01
Appendix A 191 AE-52-800-04-01Appendix A 192 AE-52-800-04-01Appendix A 193 AE-52-800-04-01Appendix A 194 AE-52-800-04-01Appendix A 195 53-TNK-01-01Appendix A 196 53-TNK-01-01Appendix A 197 53-TNK-02-01Appendix A 198 53-TNK-02-01Appendix A 199 53-TNK-02-02Appendix A 200 53-TNK-02-02Appendix A 201 AE-53-037-01-01Appendix A 202 AE-53-037-01-01Appendix A 203 AE-53-037-01-01Appendix A 204 AE-53-037-01-01Appendix A 205 AE-53-037-01-01Appendix A 206 AE-53-037-01-01Appendix A 207 AE-53-037-01-01Appendix A 208 AE-53-037-01-01Appendix A 209 AE-53-037-01-01Appendix A 210 AE-53-037-01-01Appendix A 211 AE-53-037-01-01Appendix A 212 AE-53-037-01-01Appendix A 213 AE-53-037-01-01Appendix A 214 AE-53-037-01-01Appendix A 215 AE-53-037-02-01Appendix A 216 AE-53-037-02-01Appendix A 217 AE-53-037-02-01Appendix A 218 AE-53-037-02-01Appendix A 219 AE-53-050-01-01Appendix A 220 AE-53-050-01-01Appendix A 221 AE-53-050-02-01Appendix A 222 AE-53-050-02-01Appendix A 223 AE-53-050-03-01Appendix A 224 AE-53-050-03-01Appendix A 225 AE-53-050-03-01Appendix A 226 AE-53-050-03-01Appendix A 227 AE-53-050-03-01Appendix A 228 AE-53-050-03-01
Rev 0 19 March 2014
Appendix A LEP-4
List of Effective Pages - Appendix A
Ch. # Page # Card # Ch. # Page # Card #
MD-80 MAINTENANCE MANUAL
Appendix A 229 AE-53-050-03-01Appendix A 230 AE-53-050-03-01Appendix A 231 AE-53-050-03-01Appendix A 232 AE-53-050-03-01Appendix A 233 AE-53-050-03-01Appendix A 234 AE-53-050-03-01Appendix A 235 AE-53-050-03-01Appendix A 236 AE-53-050-03-01Appendix A 237 AE-53-050-04-01Appendix A 238 AE-53-050-04-01Appendix A 239 AE-53-050-04-01Appendix A 240 AE-53-050-04-01Appendix A 241 AE-53-050-04-01Appendix A 242 AE-53-050-04-01Appendix A 243 AE-53-050-05-01Appendix A 244 AE-53-050-05-01Appendix A 245 AE-53-050-05-01Appendix A 246 AE-53-050-05-01Appendix A 247 AE-53-050-05-01Appendix A 248 AE-53-050-05-01Appendix A 249 AE-53-050-05-01Appendix A 250 AE-53-050-05-01Appendix A 251 AE-53-050-05-01Appendix A 252 AE-53-050-05-01Appendix A 253 AE-53-050-05-01Appendix A 254 AE-53-050-05-01Appendix A 255 AE-53-050-05-01Appendix A 256 AE-53-050-05-01Appendix A 257 AE-53-050-06-01Appendix A 258 AE-53-050-06-01Appendix A 259 AE-53-050-06-01Appendix A 260 AE-53-050-06-01Appendix A 261 AE-53-050-06-01Appendix A 262 AE-53-050-06-01Appendix A 263 AE-53-050-06-01Appendix A 264 AE-53-050-06-01Appendix A 265 AE-53-050-06-01Appendix A 266 AE-53-050-06-01
Appendix A 267 AE-53-050-06-01Appendix A 268 AE-53-050-06-01Appendix A 269 AE-53-050-06-01Appendix A 270 AE-53-050-06-01Appendix A 271 AE-53-050-06-01Appendix A 272 AE-53-050-06-01Appendix A 273 AE-53-050-06-01Appendix A 274 AE-53-050-06-01Appendix A 275 AE-53-050-07-01Appendix A 276 AE-53-050-07-01Appendix A 277 AE-53-050-07-01Appendix A 278 AE-53-050-07-01Appendix A 279 AE-53-050-07-01Appendix A 280 AE-53-050-07-01Appendix A 281 AE-53-050-07-01Appendix A 282 AE-53-050-07-01Appendix A 283 AE-53-051-01-01Appendix A 284 AE-53-051-01-01
Rev 0 19 March 2014
Appendix A-1
MD-80 MAINTENANCE MANUAL
Appendix A
���������� ��
� ������ ����� �����
�� �� ���������������������
�� � ������������������
��� ������
������� �
��������� �� �� � �� ���
����
�! �!���
������
����
������
������������ ����� ��"���������� #������$
����� ����� �����
���������� � ��"�
���!��� ���
���
�����
%����$�
������������������ � ��� &'(((�
�"���������
������
��������� � ������ �������������������� �������������������������������������������
���� ���
Appendix A-2
MD-80 MAINTENANCE MANUAL
Intentionally Left Blank
Appendix A-3
MD-80 MAINTENANCE MANUAL
���������� ��
� ������ ����� �����
��������� ������������ ��
�� � ������������������
��� �����
������� �
�������� � �� � �� ���
����
�� �����
������
���
������
��������� ���� �������
������ ��������
����� ����� ����
��������� � ����
������ ���
���
�����
)������
������������������ � ��� ������
����������
������
������������������������������������������ ��������������������������������������!$��
���� ���
Appendix A-4
MD-80 MAINTENANCE MANUAL
Intentionally Left Blank
Appendix A-5
MD-80 MAINTENANCE MANUAL
���������� ��
� ������ ����� �����
������������������������� �� ���������������
�� � ����� ������� ����
��� ������
������� �
��������� �� �� � �� ���
����
� ����
������� �� �����
����
������� �� ����
������������ ����� �������
����� ����� ��
����� ����� �����
���������� � ����
������ ��
���
�����
%������
��������������� � �� ������
����������
�������������������������� �������������������������������������������������������������������� �*�
���;�
��<>��<�?��@Q��[\<���]�^<Q��������`�{��� ����@|}}��>~>Q��*� �����������*�\�����{��� � ��@}��@|}}��<�>Q�||�Q<}�*�
���� ���
Appendix A-6
MD-80 MAINTENANCE MANUAL
Intentionally Left Blank
Appendix A-7
MD-80 MAINTENANCE MANUAL
MD-80 TASK CARD
AIRLINE CARD NO. TITLE
WALKTHROUGH AND VISUAL INSPECTION
EAC CARD NO. 25-TNK-02-02
DATE TASK INS
RELATED CARD
TAIL NUMBER WORK AREA VERSION
Org
THRESHOLD
N/A
REPEAT
125 CYC
APPLICABILITY AIRPLANE ENGINES MD-80 JT8D-219
STATION SKILLAIRPLANE
BODY STATION STRINGER
ATA CHAPTER 25
ACCESS
NOTE
ZONE 51
FLEET EFFECTIVITY AIRCRAFT 73444
PAGE 1 OF 3
NOTE:
Unload ULD’s (pallets) in accordance with ANCRA CMM 25-51-67 pg 6 (inspect ULD per CMM 25-50-00 and cargo nets per CMM 25-55-11).
Accomplish the following:
Doorsill Protector:
Make sure the doorsill protector is operative and can be lowered and stowed properly. Inspect all equipment on the doorsill such as rollers and side guides for proper functionality (verify by operating the equipment).
Walkthrough and visual inspection
The purpose of this inspection is to identify obvious missing or broken LRUs to ensure loading is safe and complies with intended function of the cargo system.
Before loading, walk through the main deck and inspect that all locks are installed. Inspect that the end stops are installed.
Inspect all side guides to ensure that they are not damaged to result in ULD getting jammed.
Appendix A-8
MD-80 MAINTENANCE MANUAL
MD-80
TASK CARDAIRLINE CARD NO. TITLE
WALKTHROUGH AND VISUAL INSPECTION
EAC CARD NO.25-TNK-02-02
DATE TASKINS
RELATED CARD
TAIL NUMBER WORK AREA VERSION
Org
THRESHOLD
N/A
REPEAT
125 CYC
APPLICABILITYAIRPLANE ENGINES
MD-80 JT8D-219
STATION SKILLAIRPLANE
BODY STATION STRINGER
ATA CHAPTER 25
ACCESS
NOTE
ZONE 51
FLEET EFFECTIVITYAIRCRAFT 73444
PAGE 2 OF 3
Inspect that the ball mat surface is clean and if any ball units are missing. Inspectthe roller conveyance system for missing or broken rollers. Although missingrollers and ball units do not constitute missing restraint condition, but large areawithout roller/ball support impact the functionality of the cargo system andincrease the system rolling friction due to ULD sagging. Therefore followingloading limitation shall apply:
ULD cannot be parked and locked in a position where more than 10% ofthe ball units are missing in this area.
ULD cannot be parked and locked in a position where more than 10% ofthe rollers are missing in this area.
Make sure MDCLS is free from foreign objects. Remove cord, plastic wrap, ice,liquid, animal waste, and trash from around components. Remove any liquidthat has flowed around components. This is important to prevent corrosion.Inspect aircraft floor and seat tracks for loose fasteners, if loose fasteners arefound, check if they belong to the cargo equipment. If the fastener belongs to cargo
equipment, consult CMM/IPL 25-51-67 to repair or replace the damagedcomponent.
Missing or Broken RestraintIf any of the restraint devices is damaged (missing or broken), ULD weight atthat position is either reduced or the position must be void. Refer to W&B fordisposition. In case of any doubt or lack of information, a position with brokenor missing restraint MUST stay void.
Appendix A-9
MD-80 MAINTENANCE MANUAL
MD-80 TASK CARD
AIRLINE CARD NO. TITLE
WALKTHROUGH AND VISUAL INSPECTION
EAC CARD NO. 25-TNK-02-02
DATE TASK INS
RELATED CARD
TAIL NUMBER WORK AREA VERSION
Org
THRESHOLD
N/A
REPEAT
125 CYC
APPLICABILITY AIRPLANE ENGINES MD-80 JT8D-219
STATION SKILLAIRPLANE
BODY STATION STRINGER
ATA CHAPTER 25
ACCESS
NOTE
ZONE 51
FLEET EFFECTIVITY AIRCRAFT 73444
PAGE 3 OF 3
Inspect pallet 463L for serviceability per CMM 25-50-00.
Inspect cargo nets for serviceability per CMM 25-55-11.
After inspection, install ULD (pallets) in accordance with ANCRA CMM 25-51-67 pg 6 paragraph F.
Return cargo floor installation back to service.
REF:
ANCRA CMM 25-51-67
ANCRA Report number 9682. T.O. 35D33-2-2-2.
Appendix A-10
MD-80 MAINTENANCE MANUAL
Intentionally Left Blank
Appendix A-11
MD-80 MAINTENANCE MANUAL
Appendix A-12
MD-80 MAINTENANCE MANUAL
Appendix A-13
MD-80 MAINTENANCE MANUAL
Appendix A-14
MD-80 MAINTENANCE MANUAL
Appendix A-15
MD-80 MAINTENANCE MANUAL
Appendix A-16
MD-80 MAINTENANCE MANUAL
Appendix A-17
MD-80 MAINTENANCE MANUAL
Appendix A-18
MD-80 MAINTENANCE MANUAL
Intentionally Left Blank
Appendix A-19
MD-80 MAINTENANCE MANUAL
Appendix A-20
MD-80 MAINTENANCE MANUAL
Appendix A-21
MD-80 MAINTENANCE MANUAL
Appendix A-22
MD-80 MAINTENANCE MANUAL
Intentionally Left Blank
Appendix A-23
MD-80 MAINTENANCE MANUAL
Appendix A-24
MD-80 MAINTENANCE MANUAL
Appendix A-25
MD-80 MAINTENANCE MANUAL
Appendix A-26
MD-80 MAINTENANCE MANUAL
Intentionally Left Blank
Appendix A-27
MD-80 MAINTENANCE MANUAL
Appendix A-28
MD-80 MAINTENANCE MANUAL
Appendix A-29
MD-80 MAINTENANCE MANUAL
Appendix A-30
MD-80 MAINTENANCE MANUAL
Intentionally Left Blank
Appendix A-31
MD-80 MAINTENANCE MANUAL
Appendix A-32
MD-80 MAINTENANCE MANUAL
Appendix A-33
MD-80 MAINTENANCE MANUAL
Appendix A-34
MD-80 MAINTENANCE MANUAL
Intentionally Left Blank
Appendix A-35
MD-80 MAINTENANCE MANUAL
Appendix A-36
MD-80 MAINTENANCE MANUAL
Appendix A-37
MD-80 MAINTENANCE MANUAL
Appendix A-38
MD-80 MAINTENANCE MANUAL
Intentionally Left Blank
Appendix A-39
MD-80 MAINTENANCE MANUAL
Appendix A-40
MD-80 MAINTENANCE MANUAL
Appendix A-41
MD-80 MAINTENANCE MANUAL
Appendix A-42
MD-80 MAINTENANCE MANUAL
Intentionally Left Blank
Appendix A-43
MD-80 MAINTENANCE MANUAL
Appendix A-44
MD-80 MAINTENANCE MANUAL
Appendix A-45
MD-80 MAINTENANCE MANUAL
Appendix A-46
MD-80 MAINTENANCE MANUAL
Intentionally Left Blank
Appendix A-47
MD-80 MAINTENANCE MANUAL
Appendix A-48
MD-80 MAINTENANCE MANUAL
Appendix A-49
MD-80 MAINTENANCE MANUAL
Appendix A-50
MD-80 MAINTENANCE MANUAL
Intentionally Left Blank
Appendix A-51
MD-80 MAINTENANCE MANUAL
Appendix A-52
MD-80 MAINTENANCE MANUAL
Appendix A-53
MD-80 MAINTENANCE MANUAL
Appendix A-54
MD-80 MAINTENANCE MANUAL
Appendix A-55
MD-80 MAINTENANCE MANUAL
Appendix A-56
MD-80 MAINTENANCE MANUAL
Intentionally Left Blank
Appendix A-57
MD-80 MAINTENANCE MANUAL
Appendix A-58
MD-80 MAINTENANCE MANUAL
Appendix A-59
MD-80 MAINTENANCE MANUAL
Appendix A-60
MD-80 MAINTENANCE MANUAL
Appendix A-61
MD-80 MAINTENANCE MANUAL
Appendix A-62
MD-80 MAINTENANCE MANUAL
Appendix A-63
MD-80 MAINTENANCE MANUAL
Appendix A-64
MD-80 MAINTENANCE MANUAL
Intentionally Left Blank
Appendix A-65
MD-80 MAINTENANCE MANUAL
Appendix A-66
MD-80 MAINTENANCE MANUAL
Appendix A-67
MD-80 MAINTENANCE MANUAL
Appendix A-68
MD-80 MAINTENANCE MANUAL
Appendix A-69
MD-80 MAINTENANCE MANUAL
Appendix A-70
MD-80 MAINTENANCE MANUAL
Intentionally Left Blank
Appendix A-71
MD-80 MAINTENANCE MANUAL
Appendix A-72
MD-80 MAINTENANCE MANUAL
Appendix A-73
MD-80 MAINTENANCE MANUAL
Appendix A-74
MD-80 MAINTENANCE MANUAL
Intentionally Left Blank
Appendix A-75
MD-80 MAINTENANCE MANUAL
Appendix A-76
MD-80 MAINTENANCE MANUAL
Appendix A-77
MD-80 MAINTENANCE MANUAL
Appendix A-78
MD-80 MAINTENANCE MANUAL
Appendix A-79
MD-80 MAINTENANCE MANUAL
Appendix A-80
MD-80 MAINTENANCE MANUAL
Appendix A-81
MD-80 MAINTENANCE MANUAL
Appendix A-82
MD-80 MAINTENANCE MANUAL
Appendix A-83
MD-80 MAINTENANCE MANUAL
Appendix A-84
MD-80 MAINTENANCE MANUAL
Appendix A-85
MD-80 MAINTENANCE MANUAL
Appendix A-86
MD-80 MAINTENANCE MANUAL
Intentionally Left Blank
Appendix A-87
MD-80 MAINTENANCE MANUAL
Appendix A-88
MD-80 MAINTENANCE MANUAL
Appendix A-89
MD-80 MAINTENANCE MANUAL
Appendix A-90
MD-80 MAINTENANCE MANUAL
Appendix A-91
MD-80 MAINTENANCE MANUAL
Appendix A-92
MD-80 MAINTENANCE MANUAL
Appendix A-93
MD-80 MAINTENANCE MANUAL
Appendix A-94
MD-80 MAINTENANCE MANUAL
Appendix A-95
MD-80 MAINTENANCE MANUAL
Appendix A-96
MD-80 MAINTENANCE MANUAL
Appendix A-97
MD-80 MAINTENANCE MANUAL
Appendix A-98
MD-80 MAINTENANCE MANUAL
Appendix A-99
MD-80 MAINTENANCE MANUAL
Appendix A-100
MD-80 MAINTENANCE MANUAL
Appendix A-101
MD-80 MAINTENANCE MANUAL
Appendix A-102
MD-80 MAINTENANCE MANUAL
Appendix A-103
MD-80 MAINTENANCE MANUAL
Appendix A-104
MD-80 MAINTENANCE MANUAL
Appendix A-105
MD-80 MAINTENANCE MANUAL
Appendix A-106
MD-80 MAINTENANCE MANUAL
Appendix A-107
MD-80 MAINTENANCE MANUAL
Appendix A-108
MD-80 MAINTENANCE MANUAL
Appendix A-109
MD-80 MAINTENANCE MANUAL
Appendix A-110
MD-80 MAINTENANCE MANUAL
Appendix A-111
MD-80 MAINTENANCE MANUAL
Appendix A-112
MD-80 MAINTENANCE MANUAL
Appendix A-113
MD-80 MAINTENANCE MANUAL
Appendix A-114
MD-80 MAINTENANCE MANUAL
Appendix A-115
MD-80 MAINTENANCE MANUAL
Appendix A-116
MD-80 MAINTENANCE MANUAL
Appendix A-117
MD-80 MAINTENANCE MANUAL
Appendix A-118
MD-80 MAINTENANCE MANUAL
Appendix A-119
MD-80 MAINTENANCE MANUAL
Appendix A-120
MD-80 MAINTENANCE MANUAL
Appendix A-121
MD-80 MAINTENANCE MANUAL
Appendix A-122
MD-80 MAINTENANCE MANUAL
Appendix A-123
MD-80 MAINTENANCE MANUAL
Appendix A-124
MD-80 MAINTENANCE MANUAL
Appendix A-125
MD-80 MAINTENANCE MANUAL
Appendix A-126
MD-80 MAINTENANCE MANUAL
Appendix A-127
MD-80 MAINTENANCE MANUAL
Appendix A-128
MD-80 MAINTENANCE MANUAL
Appendix A-129
MD-80 MAINTENANCE MANUAL
Appendix A-130
MD-80 MAINTENANCE MANUAL
Intentionally Left Blank
Appendix A-131
MD-80 MAINTENANCE MANUAL
Appendix A-132
MD-80 MAINTENANCE MANUAL
Appendix A-133
MD-80 MAINTENANCE MANUAL
Appendix A-134
MD-80 MAINTENANCE MANUAL
Intentionally Left Blank
Appendix A-135
MD-80 MAINTENANCE MANUAL
Appendix A-136
MD-80 MAINTENANCE MANUAL
Appendix A-137
MD-80 MAINTENANCE MANUAL
Appendix A-138
MD-80 MAINTENANCE MANUAL
Intentionally Left Blank
Appendix A-139
MD-80 MAINTENANCE MANUAL
Appendix A-140
MD-80 MAINTENANCE MANUAL
Appendix A-141
MD-80 MAINTENANCE MANUAL
Appendix A-142
MD-80 MAINTENANCE MANUAL
Appendix A-143
MD-80 MAINTENANCE MANUAL
Appendix A-144
MD-80 MAINTENANCE MANUAL
Appendix A-145
MD-80 MAINTENANCE MANUAL
Appendix A-146
MD-80 MAINTENANCE MANUAL
Intentionally Left Blank
Appendix A-147
MD-80 MAINTENANCE MANUAL
Appendix A-148
MD-80 MAINTENANCE MANUAL
Appendix A-149
MD-80 MAINTENANCE MANUAL
Appendix A-150
MD-80 MAINTENANCE MANUAL
Intentionally Left Blank
Appendix A-151
MD-80 MAINTENANCE MANUAL
Appendix A-152
MD-80 MAINTENANCE MANUAL
Appendix A-153
MD-80 MAINTENANCE MANUAL
Appendix A-154
MD-80 MAINTENANCE MANUAL
Intentionally Left Blank
Appendix A-155
MD-80 MAINTENANCE MANUAL
Appendix A-156
MD-80 MAINTENANCE MANUAL
Appendix A-157
MD-80 MAINTENANCE MANUAL
Appendix A-158
MD-80 MAINTENANCE MANUAL
Intentionally Left Blank
Appendix A-159
MD-80 MAINTENANCE MANUAL
Appendix A-160
MD-80 MAINTENANCE MANUAL
Appendix A-161
MD-80 MAINTENANCE MANUAL
Appendix A-162
MD-80 MAINTENANCE MANUAL
Intentionally Left Blank
Appendix A-163
MD-80 MAINTENANCE MANUAL
Appendix A-164
MD-80 MAINTENANCE MANUAL
Appendix A-165
MD-80 MAINTENANCE MANUAL
Appendix A-166
MD-80 MAINTENANCE MANUAL
Appendix A-167
MD-80 MAINTENANCE MANUAL
Appendix A-168
MD-80 MAINTENANCE MANUAL
Appendix A-169
MD-80 MAINTENANCE MANUAL
Appendix A-170
MD-80 MAINTENANCE MANUAL
Appendix A-171
MD-80 MAINTENANCE MANUAL
Appendix A-172
MD-80 MAINTENANCE MANUAL
Appendix A-173
MD-80 MAINTENANCE MANUAL
Appendix A-174
MD-80 MAINTENANCE MANUAL
Intentionally Left Blank
Appendix A-175
MD-80 MAINTENANCE MANUAL
Appendix A-176
MD-80 MAINTENANCE MANUAL
Appendix A-177
MD-80 MAINTENANCE MANUAL
Appendix A-178
MD-80 MAINTENANCE MANUAL
Appendix A-179
MD-80 MAINTENANCE MANUAL
Appendix A-180
MD-80 MAINTENANCE MANUAL
Appendix A-181
MD-80 MAINTENANCE MANUAL
Appendix A-182
MD-80 MAINTENANCE MANUAL
Appendix A-183
MD-80 MAINTENANCE MANUAL
Appendix A-184
MD-80 MAINTENANCE MANUAL
Appendix A-185
MD-80 MAINTENANCE MANUAL
Appendix A-186
MD-80 MAINTENANCE MANUAL
Appendix A-187
MD-80 MAINTENANCE MANUAL
Appendix A-188
MD-80 MAINTENANCE MANUAL
Appendix A-189
MD-80 MAINTENANCE MANUAL
Appendix A-190
MD-80 MAINTENANCE MANUAL
Intentionally Left Blank
Appendix A-191
MD-80 MAINTENANCE MANUAL
Appendix A-192
MD-80 MAINTENANCE MANUAL
Appendix A-193
MD-80 MAINTENANCE MANUAL
Appendix A-194
MD-80 MAINTENANCE MANUAL
Intentionally Left Blank
Appendix A-195
MD-80 MAINTENANCE MANUAL
���������� ��
� ������ ����� �����
����������� ���� ���������
�� � ������������� �� �
��� �����
������� �
������� �� �� � �� ���
����
�� �����
����������
����
����������
����������� ����� ������
����� ��������
��������� � ����
������� ���
���
�����
)���� �
������������������ � ��� ������
���� ���� �
������
����������� ��������������� ������������������������ ��
� �������������������������������������� ���� ���! ���
� "����� ��"��#$�$"�%�&��%�'�#�������� ������$���( �������������)��*�
���� ���
Appendix A-196
MD-80 MAINTENANCE MANUAL
Intentionally Left Blank
Appendix A-197
MD-80 MAINTENANCE MANUAL
���������� ��
� ������ ����� �����
������������������� ������� �� ���
�� � ��������������� �
��� �����
������� �
��������� �� �� � �� ���
����
�� �����
����$�����
����
����$�����
������������ ����� �������
������ ������ $
����� ��������
���������� � ����
������� ��
���
�����
*���$�
��������������� � �� ������
���� ��� �
������
��������������������������������������������� ����������� ������������������������������������
���� ���
Appendix A-198
MD-80 MAINTENANCE MANUAL
Intentionally Left Blank
Appendix A-199
MD-80 MAINTENANCE MANUAL
���������� ��
� ������ ����� �����
���������������� ������� �� ���
�� � �����������������
��� �����
������� �
����� ��� �� �� � �� ���
����
� ����
����������
����
����������
������������ ����� �������
������ ��������
����� ��������
���������� � ����
������ ��
���
�����
%�����
������������������ � ��� ������
�����������
������
�� ������������������������������������������ ����������� ������������������������������������
���� ���
Appendix A-200
MD-80 MAINTENANCE MANUAL
Intentionally Left Blank
Appendix A-201
MD-80 MAINTENANCE MANUAL
Appendix A-202
MD-80 MAINTENANCE MANUAL
Appendix A-203
MD-80 MAINTENANCE MANUAL
Appendix A-204
MD-80 MAINTENANCE MANUAL
Appendix A-205
MD-80 MAINTENANCE MANUAL
Appendix A-206
MD-80 MAINTENANCE MANUAL
Appendix A-207
MD-80 MAINTENANCE MANUAL
Appendix A-208
MD-80 MAINTENANCE MANUAL
Appendix A-209
MD-80 MAINTENANCE MANUAL
Appendix A-210
MD-80 MAINTENANCE MANUAL
Appendix A-211
MD-80 MAINTENANCE MANUAL
Appendix A-212
MD-80 MAINTENANCE MANUAL
Appendix A-213
MD-80 MAINTENANCE MANUAL
Appendix A-214
MD-80 MAINTENANCE MANUAL
Intentionally Left Blank
Appendix A-215
MD-80 MAINTENANCE MANUAL
Appendix A-216
MD-80 MAINTENANCE MANUAL
Appendix A-217
MD-80 MAINTENANCE MANUAL
Appendix A-218
MD-80 MAINTENANCE MANUAL
Intentionally Left Blank
Appendix A-219
MD-80 MAINTENANCE MANUAL
Appendix A-220
MD-80 MAINTENANCE MANUAL
Appendix A-221
MD-80 MAINTENANCE MANUAL
Appendix A-222
MD-80 MAINTENANCE MANUAL
Appendix A-223
MD-80 MAINTENANCE MANUAL
Appendix A-224
MD-80 MAINTENANCE MANUAL
Appendix A-225
MD-80 MAINTENANCE MANUAL
Appendix A-226
MD-80 MAINTENANCE MANUAL
Appendix A-227
MD-80 MAINTENANCE MANUAL
Appendix A-228
MD-80 MAINTENANCE MANUAL
Appendix A-229
MD-80 MAINTENANCE MANUAL
Appendix A-230
MD-80 MAINTENANCE MANUAL
Appendix A-231
MD-80 MAINTENANCE MANUAL
Appendix A-232
MD-80 MAINTENANCE MANUAL
Appendix A-233
MD-80 MAINTENANCE MANUAL
Appendix A-234
MD-80 MAINTENANCE MANUAL
Appendix A-235
MD-80 MAINTENANCE MANUAL
Appendix A-236
MD-80 MAINTENANCE MANUAL
Appendix A-237
MD-80 MAINTENANCE MANUAL
Appendix A-238
MD-80 MAINTENANCE MANUAL
Appendix A-239
MD-80 MAINTENANCE MANUAL
Appendix A-240
MD-80 MAINTENANCE MANUAL
Appendix A-241
MD-80 MAINTENANCE MANUAL
Appendix A-242
MD-80 MAINTENANCE MANUAL
Appendix A-243
MD-80 MAINTENANCE MANUAL
Appendix A-244
MD-80 MAINTENANCE MANUAL
Appendix A-245
MD-80 MAINTENANCE MANUAL
Appendix A-246
MD-80 MAINTENANCE MANUAL
Appendix A-247
MD-80 MAINTENANCE MANUAL
Appendix A-248
MD-80 MAINTENANCE MANUAL
Appendix A-249
MD-80 MAINTENANCE MANUAL
Appendix A-250
MD-80 MAINTENANCE MANUAL
Appendix A-251
MD-80 MAINTENANCE MANUAL
Appendix A-252
MD-80 MAINTENANCE MANUAL
Appendix A-253
MD-80 MAINTENANCE MANUAL
Appendix A-254
MD-80 MAINTENANCE MANUAL
Appendix A-255
MD-80 MAINTENANCE MANUAL
Appendix A-256
MD-80 MAINTENANCE MANUAL
Intentionally Left Blank
Appendix A-257
MD-80 MAINTENANCE MANUAL
Appendix A-258
MD-80 MAINTENANCE MANUAL
Appendix A-259
MD-80 MAINTENANCE MANUAL
Appendix A-260
MD-80 MAINTENANCE MANUAL
Appendix A-261
MD-80 MAINTENANCE MANUAL
Appendix A-262
MD-80 MAINTENANCE MANUAL
Appendix A-263
MD-80 MAINTENANCE MANUAL
Appendix A-264
MD-80 MAINTENANCE MANUAL
Appendix A-265
MD-80 MAINTENANCE MANUAL
Appendix A-266
MD-80 MAINTENANCE MANUAL
Appendix A-267
MD-80 MAINTENANCE MANUAL
Appendix A-268
MD-80 MAINTENANCE MANUAL
Appendix A-269
MD-80 MAINTENANCE MANUAL
Appendix A-270
MD-80 MAINTENANCE MANUAL
Appendix A-271
MD-80 MAINTENANCE MANUAL
Appendix A-272
MD-80 MAINTENANCE MANUAL
Appendix A-273
MD-80 MAINTENANCE MANUAL
Appendix A-274
MD-80 MAINTENANCE MANUAL
Appendix A-275
MD-80 MAINTENANCE MANUAL
Appendix A-276
MD-80 MAINTENANCE MANUAL
Appendix A-277
MD-80 MAINTENANCE MANUAL
Appendix A-278
MD-80 MAINTENANCE MANUAL
Appendix A-279
MD-80 MAINTENANCE MANUAL
Appendix A-280
MD-80 MAINTENANCE MANUAL
Appendix A-281
MD-80 MAINTENANCE MANUAL
Appendix A-282
MD-80 MAINTENANCE MANUAL
Appendix A-283
MD-80 MAINTENANCE MANUAL
Appendix A-284
MD-80 MAINTENANCE MANUAL