Gates Learjet 35A/36A with FC-200 AutopilotFAA APPROVED AIRPLANE FLIGHT MANUAL

THIS AIRPLANE MUST BE OPERATED IN COMPLIANCE WITH THE PRESCRIBED LIMITATIONS IN SECTION 1 OF THIS MANUAL

___________________ NOTICE ___________________ This AFM is a revised issue of the original AFM dated 4-30-76. This reissue replaces all of the information in the original issue through Change 13.

SERIAL NO. _ _ _ _ _ __

N ________________

for CHIEF, AIRCRAFT CERTIFICATION PROGRAM FAA CENTRAL REGION WlCHITA, KANSAS

FM-102

Copyright 1983 GATES LEARJET CORPORATION All rights reserved

TECHNICAL PUBLICATIONS USER COMMENT SHEETThe Bombardier-Learjet Technical Publications Team is continually striving to make our publications more usable to those in the field. We welcome your comments, criticism, and suggestions concerning any Bombardier-Learjet publication. The action taken, as the result of your comments, will be noted below and a copy returned to you. This electronic form may be returned in any of the following formats: E-mailed to learjet.squawk@aero.bombardier.com (preferred) Mailed to Bombardier-Learjet Technical Publications using business reply mail (see reverse) Faxed to (316) 946-2002 A User Comment can also be created via http://www.cic.bombardier.com Click on User Comments.

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Todays Date

Publication Information Title Rev/Chg No. Chap/Sec/Sub Page No. Page Date Aircraft Information Model Serial No. Comment/Suggestion: Issue/Rev Date

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THIS SPACE RESERVED FOR LEARJET USE ONLY Date Received Assign To Action Taken:

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............. ~~~~;;;;~;;; ................................. llrljjNO POSTAGE NECESSARY IF MAILED IN THE UNITED STATES

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BUSINESS REPLY MAILPERMIT NO. 2928 POSTAGE WILL BE PAID BY ADDRESSEE

WICHITA, KS

ATTN: TECHNICAL PUBLICATIONS (MS #53) LEARJET INC PO BOX 7707 WICHITA, KS 67277-9801

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111.111 1IMPORTANTTO THE OWNER OF THIS AIRPLANETo enswe that you receive aD applicable changes to this manual, please fill in the blanks below.and mail to the address at the bottom of the page. There Is no charge for the one Flight Manual assigned to the aircraft and you will receive all changes to the assigned manual at no charge. There is, .however, a yearly subscription charge for aD Flight Manuals not assigned to the aircraft.

AmC~S~NUMBER

________________________

MAILING ADDRESS FOR CHANGES:

MAD.. THIS SHEET TO:.Gates Learjet Corporation P.O. Box 7707 WIChita, Kansas 67277

Attn: Technical Data Control Center

Learjet 35A/36A with FC-200

Temporary Changes

LOG OF TEMPORARY FLIGHT MANUAL CHANGESThis list is intended to assist the flight crew in determining the applicable AFM temporary flight manual changes for Model 35A/36A aircraft equipped with FC-200 autopilot. It is the responsibility of the aircraft owner and operator to maintain their basic AFM with the temporary changes applicable to their aircraft. Insert this list before page A.TFM # Dated3-31-81 7-8-81 7-8-81 7-8-81

Section or Page2-19 2-2 1-13 2-29

DescriptionRevised autopilot pitch monitor check. Assure pitot-static drain valves close after draining. Minimum fuel requirement for takeoff and intentional go around. Warning pertaining to fuel starvation with nose-up attitude and low fuel. (After Takeoff checklist) Warning pertaining to fuel starvation with nose-up attitude and low fuel. Go Around checklist) Note pertaining to the MSTR WARN light. Revised stabilizer trim indicator markings. Revised turbulent air penetration procedure. Adds recovery from inadvertent overspeed procedure to emergency section. Deletes recovery from inadvertent overspeed procedure from abnormal section. Seat belts and shoulder harnesses required for takeoff and landing. Disengage autopilot during recovery from inadvertent overspeed. Select 100% OXY during before starting engines checks. Revised operation of diluter-demand crew oxygen masks. Revised oxygen duration table for ZMR 100 series crew masks. Select 100% OXY during emergency descent procedure.

StatusRemoved by Chg 1. Removed by Chg 1. Removed by Chg 1. Removed by Chg 1. Removed by Chg 1. Removed by Chg 1. Removed by Chg 1. Removed by Chg 2. Removed by Chg 2. Removed by Chg 2. Removed by Chg 5. Removed by Chg 5. Removed by Chg 5. Removed by Chg 5. Removed by Chg 5. Removed by Chg 5.

7-8-81 8-18-81 8-28-81 2-5-82 2-5-82 2-5-82 83-01 3-16-83 83-02 3-18-83 83-06 9-23-83 83-09 9-23-83 83-15 9-23-83 83-17 9-23-83

2-35 2-70 1-26 4-1 3-17 4-2 1-14 3-17A 2-7 2-45 2-47 3-22

ContinuedFM-102 6-23-2008 Change 14

TFM-1

Temporary Changes TFM # Dated84-02 3-15-84 85-02 3-8-85 85-10 1-3-86 85-16 11-8-85 87-05 3-2-87 87-06 3-2-87 87-15 7-16-87 88-07 2-13-89 88-17 1-17-89 89-17 11-16-89 92-02 9-10-92 93-15 12-3-93 94-15 1-9-95 94-23 3-6-95 96-08 5-30-96 96-09 5-30-96 96-10 7-12-96 99-02 7-16-99 99-03 4-16-99 99-24 11-30-99 99-26 12-21-99

Learjet 35A/36A with FC-200

Section or Page1-3 IV 2-2 3-5 4-17 4-19 II 4-29 II 4-16 2-16 2-35 1-14 5-8 2-49 4-17 1-14 1-18B 1-20 1-18B 1-18B

DescriptionMaximum zero wing and tip fuel weight replaces maximum wing bending weight.

Status

Removed by Chg 5. Removed by Revised FUEL CMPTR light procedure. Chg 6. Engine oil and hydraulic accumulator preRemoved by flight checks. Chg 6. Current limiter failure procedure associRemoved by ated with AMK 85-1. Chg 8. Clarify operation of emergency gear Removed by extension valve. Chg 7. Clarify operation of emergency gear Removed by extension valve. Chg 7. Bleed hydraulic pressure to zero before Superseded setting battery switches off. by TFM 88-17. Removed by Pitot-static system malfunction procedure. Chg 7. Bleed hydraulic pressure to zero before Removed by setting battery switches off. Chg 9. Fuel imbalance during fuel transfer proceRemoved by dure. Chg 9. Removed by Clarify the oil pressure annunciator. Chg 10. Removed by Cold weather operations. Chg 10. Maximum operating altitude 41,000 FT. Active, until (When cabin outflow or safety valve has SB 35/36-21-19 been replaced between 1-1-89 and 1-9-95) is accomplished. Removed by Revised noise level compliance statement. Chg 10. Removed by Standby fuel pump annunciators. Chg 10. Procedure for standby fuel pump failing Removed by to shut off. Chg 10. Adds paved runway restriction to limitaRemoved by tions section. Chg 10. Superseded by Revises the list of approved oils. TFM 99-24. Revises fuel anti-icing additive Removed by limitations. Chg 12. Superseded by Revises the list of approved oils. TFM 99-26. Removed by Revises the list of approved oils. Chg 12.

Continued

TFM-2

FM-102 6-23-2008 Change 14

Learjet 35A/36A with FC-200 TFM # Dated2001-15 4-13-01 2007-02 6-14-07 2007-04 6-14-07 2007-13 1-14-08 2007-14 1-14-08

Temporary Changes

Section or Page4-44 3-46 4-27 4-9 3-8

DescriptionRevises Single Engine Landing procedure. Revises Stall Warning Activates procedure. Revises AUG AIL Light Illuminated procedure. Revises Single Generator Failure procedure. Revises Dual Generator Failure procedure.

StatusRemoved by Chg 13. Removed by Chg 14. Removed by Chg 14. Removed by Chg 14. Removed by Chg 14.

FM-102 6-23-2008 Change 14

TFM-3

Learjet 35/36 AFM

List of Effective Pages

LIST OF EFFECTIVE PAGESUse this List of Effective Pages to determine the current status of the Airplane Flight Manual. Pages affected by the current change are indicated by an asterisk (*) immediately preceding the page number.

Learjet 35A/36A with FC-200 Autopilot AFM Dates of issue for Original and Changed pages are: Original......... O ....... 4-30-1976 Change......... 7 ........ 6-20-1989 Reissue .................... 2-25-1981 Change......... 8 ........ 1-12-1990 Change......... 1........ 9-10-1981 Change......... 9 ........ 2-20-1992 Change......... 2........ 6-24-1982 Change........ 10 ....... 3-14-1997 Change......... 3........ 1-26-1983 Change........ 11 ..... 11-18-1998 Change......... 4.......... 8-6-1984 Change........ 12 ....... 12-1-2000 Change......... 5........ 11-7-1984 Change........ 13 ......... 9-5-2006 Change......... 6........ 6-27-1986 Change........ 14 ....... 6-23-2008NOTE

This change supersedes and incorporates TFM 2007-02, TFM 2007-04, TFM 2007-13, and TFM 2007-14. Remove superseded temporary changes from AFM.Change Page Change

Page

Title ........................................ 5 * A thru C................................ 14 i ........................................... 10 ii.................................. Reissued iii thru v ................................ 10 Limitations I-1........................................ 10 I-2........................................ 13 I-312 1-1 ....................................... 13 1-2 thru 1-4 ............................ 6 1-5 ....................................... 10 1-6 thru 1-8 ................. Reissued 1-9 ....................................... 13

1-10 ....................................... 6 1-11 thru 1-14 ...................... 10 1-15 ....................................... 6 1-16 ..................................... 10 1-17 ....................................... 9 1-18 ..................................... 10 1-18A ................................... 10 1-18B and 1-18C .................. 13 1-19 ..................................... 13 1-20 thru 1-24 ...................... 12 1-25 ............................ Reissued 1-26 ....................................... 5 1-27 ..................................... 13 1-28 ....................................... 5 1-29 and 1-30 ......................... 8

FAA Approvedfor MARGARET KLINE, MANAGER AIRCRAFT CERTIFICATION OFFICE FEDERAL AVIATION ADMINISTRATION WICHITA, KANSAS

Date

FM-102 FAA APPROVED 4-30-76 REISSUED 2-25-81, CHANGE 14

A

List of Effective Pages

Learjet 35/36 AFM

LIST OF EFFECTIVE PAGES (Cont)Learjet 35A/36A with FC-200 Autopilot AFMPage Normal Procedures II-1 and II-2 ........................... 12 II-3 ....................................... 10 *II-4 ....................................... 14 2-1 thru 2-7 .......................... 10 2-8 and 2-9........................... 11 2-10 thru 2-16 ...................... 13 2-17 ..................................... 10 2-18 ..................................... 13 2-19 thru 2-23 ...................... 10 2-24 ..................................... 12 2-25 ..................................... 10 2-26 thru 2-28 ...................... 12 2-29 and 2-30....................... 10 2-31 and 2-32....................... 11 2-33 ..................................... 10 2-34 ..................................... 11 2-35 thru 2-37 ...................... 10 2-38 and 2-39....................... 12 2-40 thru 2-51 ...................... 10 2-52 and 2-53....................... 12 2-54 and 2-55....................... 10 2-56 ..................................... 13 2-57 ..................................... 10 2-58 thru 2-63 ...................... 12 2-64 and 2-65....................... 10 2-66 and 2-67....................... 12 2-68 thru 2-85 ...................... 10 Emergency Procedures III-1 ...................................... 12 *III-2 ...................................... 14 III-3 ...................................... 10 3-1 thru 3-7 .......................... 10 *3-8 ....................................... 14 3-9 and 3-10......................... 10 3-11 thru 3-13 ...................... 12 3-14 and 3-15....................... 11 3-16 thru 3-20 ...................... 10 3-21 ..................................... 12 3-22 thru 3-26 ...................... 10 3-27 thru 3-30 ...................... 12 Change Page Change

3-31 and 3-32....................... 13 3-33 thru 3-36 ...................... 10 3-37 ..................................... 12 3-38 ..................................... 10 3-39 ..................................... 13 3-40 thru 3-44 ...................... 10 3-45 ..................................... 11 * 3-46 and 3-47....................... 14 * 3-48 (Added) ......................... 14 Abnormal Procedures IV-1 ...................................... 13 IV-2 ...................................... 12 IV-3 ...................................... 13 IV-4 ...................................... 10 4-1 thru 4-8 .......................... 10 * 4-9 ....................................... 14 4-10 ..................................... 10 4-11 and 4-12....................... 13 4-13 ..................................... 12 4-14 and 4-15....................... 10 4-16 thru 4-21 ...................... 12 4-22 thru 4-26 ...................... 10 * 4-27 ..................................... 14 4-28 thru 4-34 ...................... 10 4-35 ..................................... 12 * 4-36 ..................................... 14 4-37 and 4-38....................... 10 4-39 ..................................... 11 4-40 and 4-41....................... 10 4-42 ..................................... 13 4-43 ..................................... 10 * 4-44 ..................................... 14 4-45 thru 4-48 ...................... 11 4-49 and 4-50....................... 13

B

FM-102 FAA APPROVED 4-30-76 REISSUED 2-25-81, CHANGE 14

Learjet 35/36 AFM

List of Effective Pages

LIST OF EFFECTIVE PAGES (Cont)Learjet 35A/36A with FC-200 Autopilot AFMPage Performance Data V-1 ....................................... 10 V-2 ....................................... 12 V-3 ....................................... 13 5-1 ......................................... 9 5-2 .............................. Reissued 5-2A..................................... 13 5-3 thru 5-5 .......................... 13 5-6 thru 5-8 .......................... 10 5-9 .............................. Reissued 5-10 ....................................... 6 5-11 ....................................... 8 5-12 thru 5-23 ............. Reissued 5-24 thru 5-27 ........................ 5 5-28 ............................ Reissued 5-29 ..................................... 10 5-29A thru 5-29C.................. 10 5-30 thru 5-32 ............. Reissued 5-33 and 5-34 ......................... 5 5-35 and 5-36 ....................... 11 Change Page Change

5-37 ....................................... 9 5-37A..................................... 9 5-37B and 5-37C .................. 12 5-38 and 5-39 .............. Reissued 5-40 ....................................... 3 5-41 ............................ Reissued 5-42 and 5-43 ....................... 12 5-44 ....................................... 3 5-45 thru 5-47 ............. Reissued 5-48 and 5-49 ......................... 6 5-50 thru 5-53 ............. Reissued 5-54 ....................................... 3 5-55 thru 5-57 ............. Reissued 5-58 and 5-59 ......................... 6 5-60 thru 5-64 ............. Reissued 5-65 ..................................... 10 5-66 ..................................... 13 5-66A................................... 12 5-67 thru 5-72 ............. Reissued 5-73 and 5-74 ....................... 10

FM-102 FAA APPROVED 4-30-76 REISSUED 2-25-81, CHANGE 14

C

111.11, ......INTRODUcnONTHIS AIRPLANE FUGHT MANUAL MUST BE CARRIED IN THE AJRCHAFf AT ALL TIMES.11IEMANUAL

This manual is divided into seven basic sections as foUows: Section 1- UMITATIONS containing FAA approved operating limitations which must be observed, except where a deviation is spedficaUy authorized, during operation of the aircraft. Section n- NORMAL PROCEDURES containing FAA approved operation procedures for the aircraft and its systems which may be considemd routine in day-to-day operations.Section m EMERGENCY PROCEDURES containing FAA approved operating procedures requiring the use of special system and/or regular systerns in order to protect the occupants and the aircraft from harm during a critical condition requiring immediate response. Steps of procedures endosed in a box such as this ~ should be accomplished without the aid

r--

of the checklist.

- --

I

Section IV - ABNORMAL PROCEDURES containing FAA approved operating procedures requiring the use of special systems and/or alternate use

of regular systems whicli, if followed, wiD maintain an acceptable level of airworthiness or reduce operational risk resulting from a faiJw-e condition. Section V - PERFORMANCE containing FAA approved data defining the airaaft performance under standard performance conditions. Refer to RETENTION OF FUGHT MANUAL PERFORMANCE DATA in this Introduction.Section VI - SUPPLEMENTS containing FAA Approved Airplane Right Manual Supplements. These supplements contain operating limitations, p~, and performance data and other necessary data for aircraft conducting special operations and!or equipped with specifi: equipment requiring

the supplement.

Section VIJ- WEIGHT AND BAlANCE DATA contains data intended to assist the operator in ensuring that the aircraft is properly loaded.

FAA APPROVED 4-30-76 REISSUED 2-25-81, CHANGE 10

(h[)ljUBDlIU

II

INTRODUCTION (CONT)Section I through Section V is composed of material approved by the Federal Aviation AdmInistration and together with the FAA Approved Airplane Right Manual Supplements in Section VI constitute the FAA Approved Airplane Right Manual. Section vn (Weight and Balance Data) is not FAA approved material but is included in this manual for the operator's convenience. (Weight and Balance Data) is complete withSection in itself and includes a Ust of Effective Pages. Therefore, Section may be revised in the same manner in which the FAA Approved Airplane Flight Manual ~

vn

vn

tion is revised.REVISING 11IE MANUAL

The data presented in this manual is the result of extensive flight tests and has been approved by the Federal Aviation Administration. However, cIeveIopment does not stop with the issuance of this manual and as new pr0cedures are developed they will be forwarded to the holder of this manual. Revised material will be in the fann of Temporary Right Manual Changes or Nwnbered Changes. It is the responsibility of the operator to enswe that the Right Manual is current at all times. Therefore, it is very important that changes (temporary or nwnbered) be incorporated in the manual as soon as they are received.TEMPORARY FUGHT MANUAL CHANGES

Temporary Right Manual Changes may be issued against the Flight Manual when required. These changes generally contain material that is not so exterisive as to require a Nwnbered Change and allow l..earjet to transmit revised data to the operator faster than with the NwnbeJed Change system. Temporary Flight Manual Changes are pnnted on yellow paper and include all necessary information (Publication Affected, Description of Change, and Filing Instructions) on the change itself. Temporary Right Manual Changes are to be retained in the Flight Manual until removed by some other authority - usuaJ1y a superseding Temporary Change or a Nwnbered Change.

ii

FAA APPROVED 4-30-76

RBSSUED 2-25-81

1111111 INTRODUCTION (CONT)NUMBERED CHANGES

Numbered Changes issued against the Flight Manual differ from Temporary Flight Manual Changes in that the pages contained in the NumbeJecl Change supersede like pages in the Right Manual. Each page in a Numbered Change has a "Change" number located at the lower comer of the page immediately below the FAA APPROVED date. Portions of the text affected by the change are indicated by a vertical bar at the outer margin of the page. The vertical bars may not appear on pages that contain changes to graphs or tables. Additionally, when a "changed" page is the result of a rearrangement of material due to a change on a previous page no vertical bar will appear. The Ust of Effective Pages provides the user with a guide to establish the current effective date of each page in the Right Manual and an instruction sheet for incorporating the latest Numbeted Change into the Right Manual. Information included in the Ust of Effective Pages states the cuneot Change Number for each page, the dates of Original issue and Numbemd Changes, and the Temporary Flight Manual Changes the cummt Numbered Change supersedes. An asterisk (*) next to a page number indicates pages changed, added, or deleted by the cunent change.

3:~

Numbered Changes do not automatically supersede all outstanding Temporary Right Manual Changes. Follow instructions given in "Note" on Ust of Effective Pages to determine which Temporary Right Manual Changes to remove when incorporating a Numbered Change.

RETENTION OF FUGHT MANUAL PERFORMANCE DATAThe performance data in Section V of this manual provides performance data for all aircraft with the same model designation rather than performance data for a Specific serial number aircraft. Therefore, due to serial number changes or the incorporation of Airplane Modibtion Kits (AMK's), Airplane Accessory Kits (AAK's) or Service Bulletins, petformance charts may be issued against this Right Manual which am not applicable to the specific aircraft assigned to the Right Manual. It is pennissible to relocate performance data not applicable to your speci&: aircraft to the rear of the manual.

Retention of relocated performance data is required as all pages listed on the Ust of Effective Pages constitute a complete FAA Approved Airplane Right Manual. Additionally, even though some data may be relocated, all changes must be incorporated and the manual kept current.FAA APPROVED 4-30-76 REISSUED 2-25-81, CHANGE 10iii

~mlAUBD[]U Im~INTRODUcnON (CONT)NOTES, CAUTIONS, AND WARNINGS

111.11, al

Notes, Cautions, and Warnings are used throughout this manual to focus attention on special conditions or procedures as follows: Notes are used to highlight specific operating conditions or steps of a procedure. Cautions are used to call attention to operating procedures which, if not sbictly observed, may result in damage to equipment. Warnings are used to call attention to operating procedures which, if not sbictIy adhered to, may result in personal injury or loss of life.

OrnER PUBUCAll0NSThe foHowing is a list of learjet publications referenced in this Airplane Right Manual. Such references in this manual are made by number and do not contain any revision indication. However, such references are to be understood as "the latest: revision".AIRPLANE ACCESSORY KITS (AAK)AAK 77-8

AAK 79-4 AAK 79-10 AAK 80-2 AAK8Q-3 AAK81-1 AAK83-8 AAK86-1

Increase T~ff Gross Weight to 18,000 Pounds Installation of Conical Fan Spinner for TFE 731 Engines Installation of Wmg Fences, StaB Strips and Boundary Layer Energizers (Softflite) (Superseded by AM}{ 83-5) Increase Takeoff Gross Weight to 18,300 Pounds Increase Landing Gross Weight to 15,300 Pounds Installation of Starter Bectrical Contactors Installation of Components to Allow Variable Pitch Trim Settings at Takeoff Installation of Windshield Defog Improvement

iv

FAA APPROVED 4-30-76 REISSUED 225-81, CHANGE 10

INTRODUCTION (CONT)AIRPlANE MODIFICATION KITS (AMK) Installation of Anti-Skid and Nose Steering Interface Electrical Box AMK 76-7 Relocation of Cabin Air Disbibution Row Control Valve AMK 78-13 Installation of Split Essential Bus Elechical System AMK80-17 Installation of Current Umiter Warning and Starter Indicator Ughts AMK83-5 InstaDation of Wing Fences, Stall Ships and Boundary Layer Energizers (Softflite) (Supersedes MK 79-10) AMK85-1 Electrical Power Distribution Improvement AMK90-3 InstaUation of Emergency Pressure Control Circuit Breaker AMK 91-2 Replacement of Wmdshield Anti-ice Thermostats ENGINEERING CHANGE RECORDS (ECR) ECR 1495 ECR 2234 18,000 Pounds T.O.G.W. Takeoff Gross Weight Increase AMK 76-3

I

REID CHANGE NOTICES (FCN)FCN 89-1

Increase Altitude Urnitation for Operation of Freon Air Conditioning System

SERVICE BULLETINS (SB~ SB 35/36-21-17 SB 35/36-22-4 SB 35/36-27-7 SB 35/36-28-11 SB 35/36-32-4 Installation of Wmdshield Defog Improvement Modification of Mach Trim Computer Modification of Spoileron Computer Assembly Installation of Standby Fuel Pump Annunciators Replacement of Landing Gear Hydraulic Selector Valve

I I

FAA APPROVED 4-30-76 RBSSUED 2-25-81, CHANGE 10

v

SECTION I LIMITATIONSTABLE OF CONTENTS General Certification Status....................................................................1-1 Type of Operation ....................................................................1-1 Performance Configuration .......................................................1-1 Minimum Flight Crew................................................................1-1 Maneuvers ...............................................................................1-1 Weight and C.G. Limits Maximum Ramp Weight ............................................................1-2 Maximum Certified Takeoff Weight.............................................1-3 Maximum Zero Wing and Tip Fuel Weight ..................................1-3 Maximum Allowable Takeoff Weight...........................................1-4 Maximum Certified Landing Weight............................................1-4 Maximum Allowable Landing Weight ..........................................1-5 Center-of-Gravity Envelope........................................................1-5 Aircraft Certified for 17,000 Pounds Takeoff Weight.............1-6 (Figure 1-1) ........................................................................1-6 Aircraft Certified for 18,000 Pounds Takeoff Weight.............1-7 (Figure 1-2) ........................................................................1-7 Aircraft Certified for 18,300 Pounds Takeoff Weight.............1-8 (Figure 1-3) ........................................................................1-8 Airspeed/Mach Limits Maximum Operating Speed VMO/MMO ......................................1-9 Maneuvering Speed VA .............................................................1-9 Maximum Landing Gear Operating Speed VLO ...........................1-9 Airspeed/Mach Limits (Figure 1-4) ...........................................1-10 Maximum Landing Gear Extended Speed VLE ...........................1-11 Maximum Flap Extended Speed VFE .........................................1-11 Minimum Control Speed Air VMCA...........................................1-11 Minimum Control Speed Ground VMCG ....................................1-11 Critical Engine Failure Speed V1 ..............................................1-11 Rotation Speed VR .................................................................1-12 Takeoff Safety Speed V2 .........................................................1-12 Ambient Temperature Limits (Figure 1-4A).............................1-12

FAA APPROVED 4-30-76 REISSUED 2-25-81, CHANGE 10

I-1

TABLE OF CONTENTS (Cont) Takeoff and Landing Operational Limits Temperature Limits.................................................................1-13 Maximum Altitude ..................................................................1-13 Wind Components..................................................................1-13 Runway Conditions.................................................................1-13 Maximum Nose Wheel Steering Speed .....................................1-13 Tire Limiting Speed ................................................................1-13 Tip Tank Fuel.........................................................................1-13 Minimum Fuel ........................................................................1-13 Pressurization.........................................................................1-14 Seat Belts ..............................................................................1-14 Enroute Operational Limits Temperature Limits.................................................................1-14 Maximum Operating Altitude...................................................1-14 Flight Load Acceleration Limits................................................1-14 System Limits Stall Warning System ..............................................................1-15 Trim Systems .........................................................................1-15 Yaw Damper ..........................................................................1-16 Spoiler...................................................................................1-16 Hydraulic System....................................................................1-16 Generator Limits ....................................................................1-16 Electrical System ...................................................................1-17 Engine Synchronizer ...............................................................1-17 External Power.......................................................................1-17 Freon Cooling System.............................................................1-17 Oxygen System ......................................................................1-18 Pressurization Limit ............................................................. 1-18A Windshield and Radome Anti-Ice Fluid................................... 1-18A Thrust Reversers (if installed)................................................. 1-18A Powerplant Limits Engine Speed Limits .............................................................1-18B Engine Operating Temperatures.............................................1-18B Turbine Temperature Limits (ITT) Starting (Figure 1-5)....................................................... 1-18C Except Starting (Figure 1-6) ...............................................1-19 Oil Limits Oil Temperature ...................................................................1-18B Approved Oils ......................................................................1-18BI-2 FAA APPROVED 4-30-76 REISSUED 2-25-81, CHANGE 13

111.11, .a alTABLE OF CONTENTS (Cont)

FuelUmits

Fuel Temperature ................................................................... 1-20 Unusable Fuel ........................................................................ 1-20 Fuel Additives ......................................................................... 1-20 Anti-Icing Additive ............................................................... 1-20 Biocide Additive .................................................................. 1-20 8ectronic Fuel Computer Specific Gravity ................................ 1-21 Approved Fuels ...................................................................... 1-22Emergency Fuel

Aviation Gasoline ................................................................... 1-23Instrument Markings

AirspeedlMachmeter .............................................................. 1-25 Trim ...................................................................................... 1-26 Cabin A1timeter/Differential Pressure ....................................... 1-26 Turbine Speed (N2) ................................................................. 1-27 Turbine Temperature (1TT) ....................................................... 1-27 Fan Speed (Nl) ....................................................................... 1-28 Oil Pressure ........................................................................... 1-28 Oil Temperature ..................................................................... 1-29 Ammeter ............................................................................... 1-29 DC Voltmeter ......................................................................... 1-29 AC Voltmeter ......................................................................... 1-29 HydrauliC Pressure .................................................................. 1-30 Emergency Air ....................................................................... 1-30 Oxygen Pressure .................................................................... 1-30

FAA APPROVED 4-30-76 REISSUED 2-25-81, CHANGE 12

1-3

GENERALCERTIFICATION STATUS This airplane is certified in accordance with FAR 25. TYPE OF OPERATION This aircraft is approved for VFR, IFR, day, night, and icing conditions. When icing or frost conditions exist, this airplane must be inspected and operated in accordance with the Cold Weather Operation procedures of Section II. These procedures include the requirement to assure that all critical surfaces of the airplane (wing, vertical and horizontal stabilizers, flight control surfaces, spoilers and flaps) are free of frost, ice and snow for takeoff. Conducting only a visual inspection may not detect very small levels of contamination; therefore, a tactile (hand on surface) check of the wing leading edge and adjacent wing upper surface is required when the ambient temperature is less than 10 C (50 F). PERFORMANCE CONFIGURATION The airplane configuration must be as presented under Standard Performance Conditions in Section V. MINIMUM FLIGHT CREW The minimum flight crew shall consist of pilot and copilot. MANEUVERS No aerobatic maneuvers, including spins, are approved. Intentional stalls (pusher actuations) are prohibited above 18,000 feet with flaps and/or landing gear extended.

FAA APPROVED 4-30-76 REISSUED 2-25-81, CHANGE 13

1-1

WEIGHT AND C.G. LIMITSMAXIMUM RAMP WEIGHTNOTE

Ramp Weight shall not exceed Maximum Allowable Takeoff Weight by more than 250 lbs (113 kg).

MODEL 35A: Serials 35-067 and subsequent not incorporating ECR 1495, ECR 2234, AAK 77-8, or AAK 80-2 .... 17,250 Pounds 7,825 kg Serials 35-067 thru 35-344 when incorporating ECR 1495 or AAK 77-8 ........................................ 18,250 Pounds 8,278 kg Serials 35-067 thru 35-344 when incorporating AAK 80-2............................................................. 18,500 Pounds 8,392 kg Serials 35-345 and subsequent when incorporating ECR 2234 ............................................................. 18,500 Pounds 8,392 kg MODEL 36A: Serials 36-018 thru 36-045 not incorporating AAK 80-2 ............................................................. 18,250 Pounds 8,278 kg Serials 36-018 thru 36-045 when incorporating AAK 80-2.............................................................. 18,500 Pounds 8,392 kg Serials 36-046 and subsequent ............................. 18,500 Pounds 8,392 kg

1-2

FAA APPROVED 4-30-76 REISSUED 2-25-81, CHANGE 6

1111111 1WEIGHT AND C.G. UNITS (CONT)MAXIMUM CERTIFIED TAKEOFF WEIGHTMODEL 35A: Serials 35067 and subsequent not incorporating ECR 1495, 17,000 Pounds ECR 2234, AAK 778, or AAK 802 . . . . . . . . . . . 7,711 kg SerialS '35~067 thru 35344 when incorporating ECR 1495 orAAK 778 ................... . 18,000 Pounds 8,165 kg Serials 35067 thru 35344 when incorporating AAK802 .............................. . 18,300 Pounds 8,301 kg Serials 35345 and subsequent when incorporating ECR2234 ............................. . 18,300 Pounds 8,301 kg MODEL 36A: Serials 36018 thru 36045 not incorporating AAK802 .............................. .

I

18,000 Pounds 8,165 kg 18,300 Pounds8,301 kg 18,300 Pounds 8,301 kg 13,500 Pounds &,124 kg

Serials 36018 thru 36-045 when incorporating AAK80-2 .............................. . Serials 36-046 and subsequent ............... .

MAXIMUM ZERO WING AND TIP fUEL WEIGHT .

All weights in excess of 13,500 pounds must consist of wing and tip tank fuel, except as follows: 1. The Maximum Zero Wing and Tip Fuel Weight may be increased to 14,000 pounds by adding up to 500 pounds of additional fuselage fuel. The additional fuselage fuel must be transferred prior to reaching a total wing fuel quantity of 2250 pounds. 2. In the event the additional fuselage fuel cannot be transferred, VMO must be reduced to 325 KIAS.

FAA APPROVED 4-30-76 REISSUED 2-25-81, CHANGE 6

1-3

11....1 WEIGHT AND C.G. UNITS (CONT)MAXIMUM AU.OWABLE TAKEOFF WEIGHTThe takeoff weight is limited by the most restrictive of the following re:quirements: Maximum Certified Takeoff Weight. Maximum Takeoff Weight (Climb or Brake Energy limited) for altitude and temperature as determined from the applicable figure entitled TAKEOFF WEIGHT UMITS in Section V. Maximum Takeoff Weight for the runway and ambient conditions as determined from the applicable figure entitled TAKEOFF DlSTANCE in Section V. Maximum Takeoff Weight for obstacle clearance as determined from the applicable TAKEOFF FUGHT PATH and CUMB GRADIENT figures in Section V. (FAR 121 and 135 as applicable to U.S. registeredaircraft.)

MAXIMUM CERTIFIED lANDING WEIGHTMODEL 35A: Serials 35-067 thru 35-344 not incorporating AAKBO-3 .............................. . Serials 35-067 thru 35-344 when incorporating AAKBO-3 .......................... .... . Se~als 35-345 and subsequen~ .............. .

14,300 Pounds 6,486 kg 15,300 Pounds 6,940 kg 15,300Pounds 6,940 kg

MODEL 36A:' Serials 36-018 thru 36-045 not incorporating AAKBO-3 .............................. . Serials 36-018 thru 36-045 when incorporating

14,300 Pounds 6,486 kg 15,300 Pounds 6,940 kg 15,300 Pounds 6,940 kg

AAKBO-3 .............................. . Serials 36-046 and subsequent .............. .

1-4

FAA APPROVED 4-30-76 REISSUED 2-25-81, CHANGE 6

111.111 1WBGHT AND C.G. UMlTS (CONI')MAXIMUM AllOWABlE lANDING WEIGHTThe landing weight is limited by the most restrictive of the following requirements: Maximum Certified Landing Weight. Perform Hard or Overweight Landing Inspection (Chapter 5, 35/36/35N36A Maintenance Manual) if Maximum Certified Landing Weight is exceeded. Maximum Landing Weight for the nmway and ambient conditions as determined from the applicable lANDING DISTANCE chart in Section V. Maximum Landing Weight (Approach Climb or Brake Energy Umited) for altitude and temperature as determined from the applicable figure entitled lANDING WEIGHT UMITS in Section V. CENTER-oF-GRAVITV ENVELOPE

I

Aircraft Certified for 17,000 Pounds Takeoff Weight. The forward C.G. limit is Fuselage Station (F.S.) 366.31 (5% MAC) for all weights up to and including 10,000 pounds and tapers through ES. 375.96 (16.66% MAC) at 17,000 pounds to ES. 376.31 (17.09% MAC) at 17,250 pounds. The aft C.G. limit is ES. 387.00 (30%MAC) for all weights. Refer to Rgure 1-1.

Aircraft Certified for 18,000 Pounds Takeoff Weight. The forward C.G. limit is Fuselage Station (F.S.) 366.31 (5% MAC) for allweights up to and including 10,000 pounds and tapers through ES. 377 .34 (18.33% MAC) at 18,000 pounds to ES. 377.69 (18.76% MAC) at 18,250 pounds. The aft C.G. limit is ES. 387.00 (30% MAC) at all weights. Refer to Rgure 1-2.

Aircraft Certified for 18,300 Pounds Takeoff Weight. The forward C.G. limit is Fuselage Station (F.S.) 366.31 (5% MAC) for all weights up to and including 10,000 pounds and tapers through ES. 377.75 (18.83% MAC) at 18,300 pounds to ES. 378.03 (19.17% MAC) at 18,500 pounds. The aft C.G. limit is ES. 387.00 (30% MAC) at all weights. Refer to Figure 1-3.

FAA APPROVED 4-30-76

REISSUED 2-25-81, CHANGE 10

1-5

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AIRCRAFT CERTIFIED FOR 17,000 POUNDS TAKEOFF WEIGHT

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FAA APPROVED 4-30-76 REISSUED 2-25-81

111.11ROTATION SPEED (Va) FLAPS - 20 0EXAMPLE: 1. Weight. ......................... 15,000 LB 2. Rotation Speed .................... 127.0 K1AS

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