design change: replacement of halon 1301 lavatory fire
TRANSCRIPT
INSTRUCTIONS FOR CONTINUED AIRWORTHINESS
DOA No. EASA.21J.540
AAG-18-C107-ICA ISSUE 1
REFERENCE PROCEDURE DOP-013 & DOP-018
Form Ref No.: DOF-020 INSTRUCTIONS FOR CONTINUED
AIRWORTHINESS
Form Issue and date:
Issue 11 – APR. 2017 Page 1 of 16
Design Change: Replacement of Halon 1301 Lavatory Fire Extinguishers to
FM200 type (B737)
Project No: AAG-18-C107
Effective Aircraft:
Owner/ Operator
Aircraft Type GROUP Registration Serial Number
ASL GROUP
Boeing 737-300 (Passenger)
1 Applicable to all ASL Group aircraft
fitted with halon fire extinguisher A800100-*
Boeing 737-400 (Passenger)
Boeing 737-400 (Combi)
Boeing 737-700 (Passenger)
Boeing 737-800 (Passenger)
Boeing 737-300 (Freighter)
2
Applicable to all ASL Group aircraft fitted with halon fire extinguisher
A800100-*
Boeing 737-400 (Freighter)
Boeing 737-800 (Freighter)
The technical content of this document is approved under the authority of DOA
EASA.21J.540
This Manual or any part thereof may not be reproduced or transmitted in any form or by any means; including photocopying, electronic transfer and/or recording, without the written permission of the copyright holder, application for which should be addressed to:
Head of Design Organisation (HDO), Atlantic Aviation Group, Shannon Airport, Co. Clare Ireland
INSTRUCTIONS FOR CONTINUED AIRWORTHINESS
DOA No. EASA.21J.540
AAG-18-C107-ICA ISSUE 1
REFERENCE PROCEDURE DOP-013 & DOP-018
Form Ref No.: DOF-020 INSTRUCTIONS FOR CONTINUED
AIRWORTHINESS
Form Issue and date:
Issue 11 – APR. 2017 Page 2 of 16
1.0 Signatures
COMPILED BY
CHECKED BY
APPROVED – Head of Airworthiness (HOA)
2.0 Record of Revisions
ISSUE DATE DETAILS
2 For use at subsequent revisions
ISSUE DATE DETAILS
3 For use at subsequent revisions
INSTRUCTIONS FOR CONTINUED AIRWORTHINESS
DOA No. EASA.21J.540
AAG-18-C107-ICA ISSUE 1
REFERENCE PROCEDURE DOP-013 & DOP-018
Form Ref No.: DOF-020 INSTRUCTIONS FOR CONTINUED
AIRWORTHINESS
Form Issue and date:
Issue 11 – APR. 2017 Page 3 of 16
3.0 Contents
1.0 SIGNATURES 2
2.0 RECORD OF REVISIONS 2
3.0 CONTENTS 3
4.0 INTRODUCTION 4
5.0 REVISIONS 4
6.0 EWIS 5
7.0 AIRWORTHINESS LIMITATIONS 5
8.0 MAINTENANCE SCHEDULING RECOMMENDATIONS 5
9.0 CONTACT DETAILS 7
9.1 Technical Enquiries 7
9.2 Supply of Parts 7
9.3 Occurrence Reporting 7
10.0 APPENDIX A - LIST OF APPLICABLE PUBLICATIONS 9
11.0 APPENDIX B – ILLUSTRATED PARTS LIST SUPPLEMENT 10
12.0 APPENDIX C – AIRCRAFT MAINTENANCE MANUAL SUPPLEMENT 14
13.0 APPENDIX D – ELECTRICAL WIRING MANUAL SUPPLEMENT 15
14.0 APPENDIX E – STRUCTURE REPAIR MANUAL SUPPLEMENT 16
INSTRUCTIONS FOR CONTINUED AIRWORTHINESS
DOA No. EASA.21J.540
AAG-18-C107-ICA ISSUE 1
REFERENCE PROCEDURE DOP-013 & DOP-018
Form Ref No.: DOF-020 INSTRUCTIONS FOR CONTINUED
AIRWORTHINESS
Form Issue and date:
Issue 11 – APR. 2017 Page 4 of 16
4.0 Introduction
This Instruction for Continued Airworthiness (ICA) document has been developed using the guidelines in Appendix “H” of EASA CS 25 as required by Commission Regulation (EC) 748/2012 Part 21A Subpart D (21A.107) and CS 25.1529. This document is designed to provide aircraft technicians with sufficient information to inspect, troubleshoot, adjust, repair, test, remove, and install the components pertaining to the subject Atlantic Aviation Group (AAG) Design Change. The Appendixes to this ICA list the documents that constitute the required information considered essential for continued airworthiness of the aircraft. These manual supplements are effective for the aircraft listed on the front sheet of this document, using the Effectivity numbers stated to identify differences between each configuration. This document is also the means by which recommendations for the amendment of Maintenance Schedules and Maintenance Manuals is advised. The information in this document supplements or supersedes the original manufacturer’s maintenance manuals only in those areas listed. For limitations, procedures and other information not contained in this document, refer to the aircraft manufacturer’s maintenance manuals, illustrated parts manuals and wiring diagrams or the vendor manuals as listed in the LOAP (APPENDIX A).
5.0 Revisions
For continuous use, the revision status of this ICA must be confirmed and maintained. Refer to the Record of Revision for information relevant to changes made to this document since initial issue. Each time the Design Change holder finds it necessary to revise this document; a revision will be distributed to all users of the Design Change. Upon receipt of the revision, any publications produced on the basis of the information contained herein should be reviewed and updated accordingly. It is the responsibility of the person(s) performing maintenance on the installed system to ensure that this document is current prior to performing any maintenance in accordance with this document. The current revision number may be verified by contacting Atlantic Aviation Group Design Services.
INSTRUCTIONS FOR CONTINUED AIRWORTHINESS
DOA No. EASA.21J.540
AAG-18-C107-ICA ISSUE 1
REFERENCE PROCEDURE DOP-013 & DOP-018
Form Ref No.: DOF-020 INSTRUCTIONS FOR CONTINUED
AIRWORTHINESS
Form Issue and date:
Issue 11 – APR. 2017 Page 5 of 16
6.0 EWIS
EWIS – This Design Engineering Change has been reviewed as per the guidance provided in AMC 20-21 and AMC 20-23, and it has been determined that this Change does not necessitate a revision to EWIS ICA previously developed for this aircraft model.
7.0 Airworthiness Limitations
There are no airworthiness limitations associated with this Design Change.
8.0 Maintenance Scheduling Recommendations
The aircraft’s approved maintenance schedule not affected by this design change.
(1) Kidde Aerospace & Defense recommends that you weigh the container, on an accurate gram scale, on installation and again at intervals of five (5) years.
NOTE: The effect of the Montreal Protocol and the U.S. Environmental Protection Agency's Clean Air Act of 1990 is to ban the release of halon into the atmosphere unless it is necessary. In compliance with the preceding, Kidde Aerospace & Defense recommends that the extinguishing agent be caught, recycled, and used again.
(2) Compare the weight of the container to the weight marked on the decal. Do not use the container if the weight loss is more than the permitted limit given (Refer to Table 1).
(3) If the weight is within the limits (Refer to Table 1), return the container to service. There is no life limit applicable to the container.
(4) For containers G800100-1 thru G800100-7, mark the weight on the weight label (PN 347841).
INSTRUCTIONS FOR CONTINUED AIRWORTHINESS
DOA No. EASA.21J.540
AAG-18-C107-ICA ISSUE 1
REFERENCE PROCEDURE DOP-013 & DOP-018
Form Ref No.: DOF-020 INSTRUCTIONS FOR CONTINUED
AIRWORTHINESS
Form Issue and date:
Issue 11 – APR. 2017 Page 6 of 16
Table 1: Leading Particulars
Description or Function Data Data
Filled Weight 0.727 to 0.987 lb (327 to 447 grams)
Effective Range 6 ft³ 0.17 m³)
Extinguishing Agent, A800100-1 thru A800100-9, A825100-1 thru A825100-11, A826300-1 and A826300-2, A826700-1 and 474276
0.221 to 0.287 lb (100 to 130 grams)
Extinguishing Agent, G800100-1 thru G800100-9, G825100-1 thru G825100-11, G826300-1, G826300-2, G826700-1, 474453 and 474453-1
0.254 to 0.287 lb (115 to 130 grams)
Operating Temperature, Automatic +170°F to +177°F (+77°C to +81°C)
Capacity 9 in.³ (148 m³)
Permitted Weight Loss, A800100-1 thru A800100-9, A825100-1 thru A825100-11, A826300-1 and A826300-2, A826700-1 and 474276
10 grams, Max.
Permitted Weight Loss, G800100-1 thru G800100-9, G825100-1 thru G825100-11, G826300-1, G826300-2, G826700-1
5 grams, Max.
Permitted Weight Loss, 474453 and 474453-1
10 grams max.
Time for full discharge 3 to 15 seconds
Installation Attached mounting bracket
Life Limit No life limit if weight is in allowable limits and extinguisher has no damage. Refer to CHECK.
INSTRUCTIONS FOR CONTINUED AIRWORTHINESS
DOA No. EASA.21J.540
AAG-18-C107-ICA ISSUE 1
REFERENCE PROCEDURE DOP-013 & DOP-018
Form Ref No.: DOF-020 INSTRUCTIONS FOR CONTINUED
AIRWORTHINESS
Form Issue and date:
Issue 11 – APR. 2017 Page 7 of 16
9.0 Contact Details
9.1 Technical Enquiries
Defect reporting or queries of a general nature concerning the changed product should be directed to:
Design Services Atlantic Aviation Group, Shannon Airport, Co. Clare, Ireland Email: [email protected]
Please use Reporting Form DOF-052 provided on the next page.
9.2 Supply of Parts
Replacement parts to support the changed product may be ordered from:
Design Services Atlantic Aviation Group, Shannon Airport, Co. Clare, Ireland Email: [email protected]
9.3 Occurrence Reporting
Form DOF-052 is provided on the next page for reporting of information related to failures, malfunctions, defects or other occurrences which cause or might cause adverse effects on the continuing airworthiness of a product, part or appliance related to a Design issued by Atlantic Aviation Group Design Organisation.
INSTRUCTIONS FOR CONTINUED AIRWORTHINESS
DOA No. EASA.21J.540
AAG-18-C107-ICA ISSUE 1
REFERENCE PROCEDURE DOP-013 & DOP-018
Form Ref No.: DOF-020 INSTRUCTIONS FOR CONTINUED
AIRWORTHINESS
Form Issue and date:
Issue 11 – APR. 2017 Page 8 of 16
INSTRUCTIONS FOR CONTINUED AIRWORTHINESS
DOA No. EASA.21J.540
AAG-18-C107-ICA ISSUE 1
REFERENCE PROCEDURE DOP-013 & DOP-018
Form Ref No.: DOF-020 INSTRUCTIONS FOR CONTINUED
AIRWORTHINESS
Form Issue and date:
Issue 11 – APR. 2017 Page 9 of 16
10.0 APPENDIX A - LIST OF APPLICABLE PUBLICATIONS
The publications listed in the LOAP constitute the required information essential for continued airworthiness for the aircraft.
Document
Number Document Title
Published By/Contact
Details
Rev. / Date
(or later
approved rev.)
[1] Aircraft Maintenance
Manual (AMM) Boeing [1]
[1] Illustrated Parts Catalog
(IPC) Boeing [1]
CMM 26-25-04 CMM Disposable Fire
Extinguishers
Kidde Aerospace and
Defense
Rev 16,
30th September
2011
[1] - Consult the latest approved revision of this document with reference to the aircraft serial
number.
It is the responsibility of the owner/operator to obtain copies of all vendor manuals listed above and to make arrangements with the vendor for provision of an amendment service to same. If any of the parts or appliances for the changed product were supplied to Atlantic Aviation Group. as Buyer Furnished Equipment (BFE), then it is the responsibility of the owner/operator to register with the vendor of such items to ensure future provision of continued airworthiness documents such as service letters or bulletins.
INSTRUCTIONS FOR CONTINUED AIRWORTHINESS
DOA No. EASA.21J.540
AAG-18-C107-ICA ISSUE 1
REFERENCE PROCEDURE DOP-013 & DOP-018
Form Ref No.: DOF-020 INSTRUCTIONS FOR CONTINUED
AIRWORTHINESS
Form Issue and date:
Issue 11 – APR. 2017 Page 10 of 16
11.0 APPENDIX B – ILLUSTRATED PARTS LIST SUPPLEMENT
Figure Item
Part Number
NOMENCLATURE
Qty [1]
EFF
1
001
002
G800100-3
AAG-11-0033-001
EXTINGUISHER ASSY-FIRE
PLACARD
3
3
All
All
– not illustrated
[1] – Per Aircraft
INSTRUCTIONS FOR CONTINUED AIRWORTHINESS
DOA No. EASA.21J.540
AAG-18-C107-ICA ISSUE 1
REFERENCE PROCEDURE DOP-013 & DOP-018
Form Ref No.: DOF-020 INSTRUCTIONS FOR CONTINUED
AIRWORTHINESS
Form Issue and date:
Issue 11 – APR. 2017 Page 11 of 16
002
Figure 1:Group 1 Aircraft Configuration
INSTRUCTIONS FOR CONTINUED AIRWORTHINESS
DOA No. EASA.21J.540
AAG-18-C107-ICA ISSUE 1
REFERENCE PROCEDURE DOP-013 & DOP-018
Form Ref No.: DOF-020 INSTRUCTIONS FOR CONTINUED
AIRWORTHINESS
Form Issue and date:
Issue 11 – APR. 2017 Page 12 of 16
Figure Item
Part Number
NOMENCLATURE
Qty [2]
EFF
2
001
002
G800100-3
AAG-11-0033-001
EXTINGUISHER ASSY-FIRE
PLACARD
1
1
All
All
– not illustrated
[2] – Per Lavatory Location
INSTRUCTIONS FOR CONTINUED AIRWORTHINESS
DOA No. EASA.21J.540
AAG-18-C107-ICA ISSUE 1
REFERENCE PROCEDURE DOP-013 & DOP-018
Form Ref No.: DOF-020 INSTRUCTIONS FOR CONTINUED
AIRWORTHINESS
Form Issue and date:
Issue 11 – APR. 2017 Page 13 of 16
002
Figure 2: Group 2 Aircraft Configuration
INSTRUCTIONS FOR CONTINUED AIRWORTHINESS
DOA No. EASA.21J.540
AAG-18-C107-ICA ISSUE 1
REFERENCE PROCEDURE DOP-013 & DOP-018
Form Ref No.: DOF-020 INSTRUCTIONS FOR CONTINUED
AIRWORTHINESS
Form Issue and date:
Issue 11 – APR. 2017 Page 14 of 16
12.0 APPENDIX C – AIRCRAFT MAINTENANCE MANUAL SUPPLEMENT
No Changes
INSTRUCTIONS FOR CONTINUED AIRWORTHINESS
DOA No. EASA.21J.540
AAG-18-C107-ICA ISSUE 1
REFERENCE PROCEDURE DOP-013 & DOP-018
Form Ref No.: DOF-020 INSTRUCTIONS FOR CONTINUED
AIRWORTHINESS
Form Issue and date:
Issue 11 – APR. 2017 Page 15 of 16
13.0 APPENDIX D – ELECTRICAL WIRING MANUAL SUPPLEMENT
No Changes
INSTRUCTIONS FOR CONTINUED AIRWORTHINESS
DOA No. EASA.21J.540
AAG-18-C107-ICA ISSUE 1
REFERENCE PROCEDURE DOP-013 & DOP-018
Form Ref No.: DOF-020 INSTRUCTIONS FOR CONTINUED
AIRWORTHINESS
Form Issue and date:
Issue 11 – APR. 2017 Page 16 of 16
14.0 APPENDIX E – STRUCTURE REPAIR MANUAL SUPPLEMENT
No Changes