Learjet 35a Technical specifications

Gates Learjet

35A/36A

with

FC-200 Autopilot

FAA

APPROVED

AIRPLANE

FLIGHT

MANUAL

THIS AIRPLANE MUST BE OPERATED IN COMPLIANCE WITH THE

PRESCRIBED LIMITATIONS

SECTION 1 OF THIS

MANUAL

___________________

NOTICE

__________________

This

AFM

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.

FM-102

SERIALNO.

______

______________

for

CHIEF, AIRCRAFT CERTIFICATION PROGRAM

FAA

CENTRAL REGION

WlCHITA, KANSAS

GATES LEARJET CORPORATION

TECHNICAL PUBLICATIONS

USER COMMENT SHEET

The 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 [email protected]bardier.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.

Today’s Date

Publication Information Customer Information

Title Your Name

Rev/Chg No. Issue/Rev Date Dept/Title

Chap/Sec/Sub Mailing Address

Page No.

Page Date

Aircraft Information E-mail

Model Telephone

Serial No. Fax No.

Comment/Suggestion:

THIS SPACE RESERVED FOR LEARJET USE ONLY

Date Received Assign To Action Taken:

Answered By Date

....

FOLD HERE FIRST

....

.............

~~~~;;;;~;;;

.................................

···············llrl·j·j

BUSINESS REPLY MAIL

FIRST-CLASS MAIL PERMIT

NO.

2928 WICHITA,

POSTAGE WILL BE

PAID

BY ADDRESSEE

ATTN: TECHNICAL PUBLICATIONS (MS #53)

LEARJET INC

PO BOX 7707

WICHITA,

67277-9801

1,11"1,,,1,,1,11,,,11,,,11,1,,1,,1,11,,",,11,,11,1

..... FOLD HERE LAST.

SEAL

WITH TAPE. DO NOTSTAPI E .....

NO POSTAGE

NECESSARY

MAILED

THE

UNITED STATES

111.111

•••••

IMPORTANT

THE

OWNER

THIS

AIRPLANE

enswe

thatyou receive

applicable changes

this manual, please

fill

the

blanks below.and mail

the

address

the

bottom of

the

page.

There

charge for the

one

Flight Manual assigned

the aircraft

and

you

will

receive

all

changes

the assigned manual

charge. There is,

.however, a yearly subscription chargefor

Flight Manuals notassigned

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

FM-102 TFM-1

6-23-2008

Change 14

LOG OF TEMPORARY FLIGHT MANUAL CHANGES

This list is intended to assist the flight crew in determining the applica-

ble 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 #

Dated

Section

or Page Description Status

3-31-81 2-19 Revised autopilot pitch monitor check. Removed by

Chg 1.

7-8-81 2-2 Assure pitot-static drain valves close after

draining.

Removed by

Chg 1.

7-8-81 1-13 Minimum fuel requirement for takeoff

and intentional go around.

Removed by

Chg 1.

7-8-81 2-29

Warning pertaining to fuel starvation with

nose-up attitude and low fuel. (After Take-

off checklist)

Removed by

Chg 1.

7-8-81 2-35

Warning pertaining to fuel starvation with

nose-up attitude and low fuel. Go Around

checklist)

Removed by

Chg 1.

8-18-81 2-70 Note pertaining to the MSTR WARN light. Removed by

Chg 1.

8-28-81 1-26 Revised stabilizer trim indicator mark-

ings.

Removed by

Chg 1.

2-5-82 4-1 Revised turbulent air penetration proce-

dure.

Removed by

Chg 2.

2-5-82 3-17 Adds recovery from inadvertent over-

speed procedure to emergency section.

Removed by

Chg 2.

2-5-82 4-2 Deletes recovery from inadvertent over-

speed procedure from abnormal section.

Removed by

Chg 2.

83-01

3-16-83 1-14 Seat belts and shoulder harnesses required

for takeoff and landing.

Removed by

Chg 5.

83-02

3-18-83 3-17A Disengage autopilot during recovery from

inadvertent overspeed.

Removed by

Chg 5.

83-06

9-23-83 2-7 Select 100% OXY during before starting

engines checks.

Removed by

Chg 5.

83-09

9-23-83 2-45 Revised operation of diluter-demand crew

oxygen masks.

Removed by

Chg 5.

83-15

9-23-83 2-47 Revised oxygen duration table for ZMR

100 series crew masks.

Removed by

Chg 5.

83-17

9-23-83 3-22 Select 100% OXY during emergency

descent procedure.

Removed by

Chg 5.

Continued

Learjet 35A/36A with FC-200 Temporary Changes

FM-102 TFM-1

6-23-2008

Change 14

LOG OF TEMPORARY FLIGHT MANUAL CHANGES

This list is intended to assist the flight crew in determining the applica-

ble 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 #

Dated

Section

or Page Description Status

3-31-81 2-19 Revised autopilot pitch monitor check. Removed by

Chg 1.

7-8-81 2-2 Assure pitot-static drain valves close after

draining.

Removed by

Chg 1.

7-8-81 1-13 Minimum fuel requirement for takeoff

and intentional go around.

Removed by

Chg 1.

7-8-81 2-29

Warning pertaining to fuel starvation with

nose-up attitude and low fuel. (After Take-

off checklist)

Removed by

Chg 1.

7-8-81 2-35

Warning pertaining to fuel starvation with

nose-up attitude and low fuel. Go Around

checklist)

Removed by

Chg 1.

8-18-81 2-70 Note pertaining to the MSTR WARN light. Removed by

Chg 1.

8-28-81 1-26 Revised stabilizer trim indicator mark-

ings.

Removed by

Chg 1.

2-5-82 4-1 Revised turbulent air penetration proce-

dure.

Removed by

Chg 2.

2-5-82 3-17 Adds recovery from inadvertent over-

speed procedure to emergency section.

Removed by

Chg 2.

2-5-82 4-2 Deletes recovery from inadvertent over-

speed procedure from abnormal section.

Removed by

Chg 2.

83-01

3-16-83 1-14 Seat belts and shoulder harnesses required

for takeoff and landing.

Removed by

Chg 5.

83-02

3-18-83 3-17A Disengage autopilot during recovery from

inadvertent overspeed.

Removed by

Chg 5.

83-06

9-23-83 2-7 Select 100% OXY during before starting

engines checks.

Removed by

Chg 5.

83-09

9-23-83 2-45 Revised operation of diluter-demand crew

oxygen masks.

Removed by

Chg 5.

83-15

9-23-83 2-47 Revised oxygen duration table for ZMR

100 series crew masks.

Removed by

Chg 5.

83-17

9-23-83 3-22 Select 100% OXY during emergency

descent procedure.

Removed by

Chg 5.

Continued

Temporary Changes Learjet 35A/36A with FC-200

TFM-2 FM-102

6-23-2008

Change 14

84-02

3-15-84 1-3 Maximum zero wing and tip fuel weight

replaces maximum wing bending weight.

Removed by

Chg 5.

85-02

3-8-85 IV Revised FUEL CMPTR light procedure. Removed by

Chg 6.

85-10

1-3-86 2-2 Engine oil and hydraulic accumulator pre-

flight checks.

Removed by

Chg 6.

85-16

11-8-85 3-5 Current limiter failure procedure associ-

ated with AMK 85-1.

Removed by

Chg 8.

87-05

3-2-87 4-17 Clarify operation of emergency gear

extension valve.

Removed by

Chg 7.

87-06

3-2-87 4-19 Clarify operation of emergency gear

extension valve.

Removed by

Chg 7.

87-15

7-16-87 II Bleed hydraulic pressure to zero before

setting battery switches off.

Superseded

by TFM 88-17.

88-07

2-13-89 4-29 Pitot-static system malfunction procedure. Removed by

Chg 7.

88-17

1-17-89 II Bleed hydraulic pressure to zero before

setting battery switches off.

Removed by

Chg 9.

89-17

11-16-89 4-16 Fuel imbalance during fuel transfer proce-

dure.

Removed by

Chg 9.

92-02

9-10-92 2-16 Clarify the oil pressure annunciator. Removed by

Chg 10.

93-15

12-3-93 2-35 Cold weather operations. Removed by

Chg 10.

94-15

1-9-95 1-14

Maximum operating altitude — 41,000 FT.

(When cabin outflow or safety valve has

been replaced between 1-1-89 and 1-9-95)

Active, until

SB 35/36-21-19

is accomplished.

94-23

3-6-95 5-8 Revised noise level compliance statement. Removed by

Chg 10.

96-08

5-30-96 2-49 Standby fuel pump annunciators. Removed by

Chg 10.

96-09

5-30-96 4-17 Procedure for standby fuel pump failing

to shut off.

Removed by

Chg 10.

96-10

7-12-96 1-14 Adds paved runway restriction to limita-

tions section.

Removed by

Chg 10.

99-02

7-16-99 1-18B Revises the list of approved oils. Superseded by

TFM 99-24.

99-03

4-16-99 1-20 Revises fuel anti-icing additive

limitations.

Removed by

Chg 12.

99-24

11-30-99 1-18B Revises the list of approved oils. Superseded by

TFM 99-26.

99-26

12-21-99 1-18B Revises the list of approved oils. Removed by

Chg 12.

Continued

TFM #

Dated

Section

or Page Description Status

Temporary Changes Learjet 35A/36A with FC-200

TFM-2 FM-102

6-23-2008

Change 14

84-02

3-15-84 1-3 Maximum zero wing and tip fuel weight

replaces maximum wing bending weight.

Removed by

Chg 5.

85-02

3-8-85 IV Revised FUEL CMPTR light procedure. Removed by

Chg 6.

85-10

1-3-86 2-2 Engine oil and hydraulic accumulator pre-

flight checks.

Removed by

Chg 6.

85-16

11-8-85 3-5 Current limiter failure procedure associ-

ated with AMK 85-1.

Removed by

Chg 8.

87-05

3-2-87 4-17 Clarify operation of emergency gear

extension valve.

Removed by

Chg 7.

87-06

3-2-87 4-19 Clarify operation of emergency gear

extension valve.

Removed by

Chg 7.

87-15

7-16-87 II Bleed hydraulic pressure to zero before

setting battery switches off.

Superseded

by TFM 88-17.

88-07

2-13-89 4-29 Pitot-static system malfunction procedure. Removed by

Chg 7.

88-17

1-17-89 II Bleed hydraulic pressure to zero before

setting battery switches off.

Removed by

Chg 9.

89-17

11-16-89 4-16 Fuel imbalance during fuel transfer proce-

dure.

Removed by

Chg 9.

92-02

9-10-92 2-16 Clarify the oil pressure annunciator. Removed by

Chg 10.

93-15

12-3-93 2-35 Cold weather operations. Removed by

Chg 10.

94-15

1-9-95 1-14

Maximum operating altitude — 41,000 FT.

(When cabin outflow or safety valve has

been replaced between 1-1-89 and 1-9-95)

Active, until

SB 35/36-21-19

is accomplished.

94-23

3-6-95 5-8 Revised noise level compliance statement. Removed by

Chg 10.

96-08

5-30-96 2-49 Standby fuel pump annunciators. Removed by

Chg 10.

96-09

5-30-96 4-17 Procedure for standby fuel pump failing

to shut off.

Removed by

Chg 10.

96-10

7-12-96 1-14 Adds paved runway restriction to limita-

tions section.

Removed by

Chg 10.

99-02

7-16-99 1-18B Revises the list of approved oils. Superseded by

TFM 99-24.

99-03

4-16-99 1-20 Revises fuel anti-icing additive

limitations.

Removed by

Chg 12.

99-24

11-30-99 1-18B Revises the list of approved oils. Superseded by

TFM 99-26.

99-26

12-21-99 1-18B Revises the list of approved oils. Removed by

Chg 12.

Continued

TFM #

Dated

Section

or Page Description Status

Learjet 35A/36A with FC-200 Temporary Changes

FM-102 TFM-3

6-23-2008

Change 14

2001-15

4-13-01 4-44 Revises Single Engine Landing

procedure.

Removed by

Chg 13.

2007-02

6-14-07 3-46 Revises Stall Warning Activates proce-

dure.

Removed by

Chg 14.

2007-04

6-14-07 4-27 Revises AUG AIL Light Illuminated

procedure.

Removed by

Chg 14.

2007-13

1-14-08 4-9 Revises Single Generator Failure proce-

dure.

Removed by

Chg 14.

2007-14

1-14-08 3-8 Revises Dual Generator Failure procedure. Removed by

Chg 14.

TFM #

Dated

Section

or Page Description Status

Learjet 35A/36A with FC-200 Temporary Changes

FM-102 TFM-3

6-23-2008

Change 14

2001-15

4-13-01 4-44 Revises Single Engine Landing

procedure.

Removed by

Chg 13.

2007-02

6-14-07 3-46 Revises Stall Warning Activates proce-

dure.

Removed by

Chg 14.

2007-04

6-14-07 4-27 Revises AUG AIL Light Illuminated

procedure.

Removed by

Chg 14.

2007-13

1-14-08 4-9 Revises Single Generator Failure proce-

dure.

Removed by

Chg 14.

2007-14

1-14-08 3-8 Revises Dual Generator Failure procedure. Removed by

Chg 14.

TFM #

Dated

Section

or Page Description Status

for MARGARET KLINE, MANAGER

AIRCRAFT CERTIFICATION OFFICE

FEDERAL AVIATION ADMINISTRATION

WICHITA, KANSAS

FAA

Approved Date

Learjet 35/36 AFM List of Effective Pages

FM-102 A

FAA APPROVED 4-30-76

REISSUED 2-25-81, CHANGE 14

LIST OF EFFECTIVE PAGES

Learjet 35A/36A with FC-200 Autopilot AFM

Use 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.

Dates of issue for Original and Changed pages are:

Page Change

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

Page Change

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

Original......... O ....... 4-30-1976

Reissue .................... 2-25-1981

Change......... 1........ 9-10-1981

Change......... 2........ 6-24-1982

Change......... 3........ 1-26-1983

Change......... 4.......... 8-6-1984

Change......... 5........ 11-7-1984

Change......... 6........ 6-27-1986

Change......... 7 ........6-20-1989

Change......... 8 ........1-12-1990

Change......... 9 ........2-20-1992

Change........ 10 .......3-14-1997

Change........ 11 .....11-18-1998

Change........ 12 .......12-1-2000

Change........ 13 .........9-5-2006

Change........ 14 .......6-23-2008

This change supersedes and incorporates

TFM 2007-02, TFM 2007-04, TFM 2007-13, and

TFM 2007-14. Remove superseded temporary

changes from AFM.

NOTE

for MARGARET KLINE, MANAGER

AIRCRAFT CERTIFICATION OFFICE

FEDERAL AVIATION ADMINISTRATION

WICHITA, KANSAS

FAA

Approved Date

Learjet 35/36 AFM List of Effective Pages

FM-102 A

FAA APPROVED 4-30-76

REISSUED 2-25-81, CHANGE 14

LIST OF EFFECTIVE PAGES

Learjet 35A/36A with FC-200 Autopilot AFM

Use 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.

Dates of issue for Original and Changed pages are:

Page Change

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

Page Change

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

Original......... O ....... 4-30-1976

Reissue .................... 2-25-1981

Change......... 1........ 9-10-1981

Change......... 2........ 6-24-1982

Change......... 3........ 1-26-1983

Change......... 4.......... 8-6-1984

Change......... 5........ 11-7-1984

Change......... 6........ 6-27-1986

Change......... 7 ........6-20-1989

Change......... 8 ........1-12-1990

Change......... 9 ........2-20-1992

Change........ 10 .......3-14-1997

Change........ 11 .....11-18-1998

Change........ 12 .......12-1-2000

Change........ 13 .........9-5-2006

Change........ 14 .......6-23-2008

This change supersedes and incorporates

TFM 2007-02, TFM 2007-04, TFM 2007-13, and

TFM 2007-14. Remove superseded temporary

changes from AFM.

NOTE

List of Effective Pages Learjet 35/36 AFM

BFM-102

FAA APPROVED 4-30-76

REISSUED 2-25-81, CHANGE 14

LIST OF EFFECTIVE PAGES (Cont)

Learjet 35A/36A with FC-200 Autopilot AFM

Page Change

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

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

List of Effective Pages Learjet 35/36 AFM

BFM-102

FAA APPROVED 4-30-76

REISSUED 2-25-81, CHANGE 14

LIST OF EFFECTIVE PAGES (Cont)

Learjet 35A/36A with FC-200 Autopilot AFM

Page Change

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

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

FM-102 C

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 AFM

Page Change

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

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 C

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 AFM

Page Change

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

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

111.11,

......

INTRODUcnON

THIS

AIRPLANE

FUGHT

MANUAL

MUST

CARRIED

THE

AJR-

CHAFf

ALL

TIMES.

11IEMANUAL

This manual is

divided

into seven basic sections as

foUows:

Section

UMITATIONS

containing

FAA

approved

operating limitations

which

must beobserved, except where a deviation is

spedficaUy

authorized,

during operation ofthe

aircraft.

Section n-

NORMAL

PROCEDURES

containing

FAA

approved opera-

tion procedures for the

aircraft

and

its

systems

which

may

be considemd

routine

day-to-day operations.

Section m-

EMERGENCY

PROCEDURES

containing

FAA

approved op-

erating procedures requiring the use of

special

system and/or

regular

sys-

terns

order to protect the occupants

and

the aircraft

from

harm during a

critical

condition requiring immediate response. Steps of procedures en-

dosed in a box

such

this

r--

should

be accomplished

without

the aid I

of the checklist. • -

Section

ABNORMAL

PROCEDURES

containing

FAA

approved op-

erating procedures requiringthe use of

special

systemsand/oralternate use

of regular systems

whicli,

followed,

wiD

maintain anacceptable

level

of air-

worthiness or

reduce

operational

risk

resulting

from

faiJw-e

condition.

Section V-

PERFORMANCE

containing

FAA

approved data

defining

the

airaaft performance under

standard

performance conditions.

Refer

RE-

TENTION

OF FUGHT

MANUAL

PERFORMANCE

DATA

this

Introduction.

Section

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

re-

quiring the supplement.

Section

VIJ-

WEIGHT

AND

BAlANCE

DATA

contains data intended to

assist

the operator

ensuring that the

aircraft

is properly loaded.

FAA

APPROVED

4-30-76

REISSUED

2-25-81,

CHANGE

(h[)ljUBDlIU

INTRODUCTION (CONT)

Section Ithrough Section V

composed of material approved by the

Fed-

eral

Aviation

AdmInistration

and

together

with

the

FAA

Approved Airplane

Right

Manual

Supplements

Section

constitute the

FAA

Approved

Air-

plane Right

Manual.

Section

(Weight

and Balance

Data)

is not

FAA

ap-

proved material but

included

this manual

for

the operator's

convenience.

Section

(Weight

and

Balance

Data)

is complete with-

itself

and includes a Ust of

Effective

Pages.

There-

fore, Section

may

revised

the same mannerin

which the

FAA

Approved Airplane

Flight

Manual

tion is

revised.

REVISING

11IE

MANUAL

The data presented in this manual is the result of extensive

flight

tests and

hasbeenapproved

the

Federal

Aviation

Administration.

However,

cIeveI-

opment does not stop with the issuance of this manual and as new

pr0ce-

dures are developed they will be forwarded to the holder of this manual.

Revised

material

will

the fann

Temporary Right

Manual

Changes

or Nwnbered Changes.

is the

responsibility

the operator to

enswe

that

the Right

Manual

is current at

all

times. Therefore,

is very important that

changes(temporary

nwnbered)

be incorporated

the manual as soonas

they are received.

TEMPORARY

FUGHT

MANUAL CHANGES

Temporary Right

Manual

Changesmay

issued

against the

Flight

Manual

when required. These changes

generally

contain material that is not so

ex-

terisive

as to require a Nwnbered Change and

allow

l..earjet to transmit

re-

vised

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 tobe retained

the

Flight

Manual

until

removed

some other

author-

ity

usuaJ1y

a superseding Temporary Change or a Nwnbered Change.

FAA

APPROVED

4-30-76

RBSSUED

2-25-81

1111111

••••••

INTRODUCTION

(CONT)

NUMBERED CHANGES

Numbered

Changes

issued

againstthe

Flight

Manual

differ

from

Temporary

Flight

Manual

Changes

that the pages contained

the

NumbeJecl

Change supersede

pages

the Right

Manual.

Each page

Num-

bered Change

has

a "Change" number located at the

lower

comer

the

page immediately

below

the

FAA

APPROVED

date. Portions ofthe text

af-

fected by the change are indicated by a

vertical

bar

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

establish

the

current effective date of each page

the Right

Manual

and an instruction

sheet

for

incorporatingthe

latest

Numbeted Change into theRight

Manual.

Information included

the

Ust

Effective

Pagesstates 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.

asterisk

(*)

next to a page number indicates pages changed,

added,

or deleted by the cunent change.

3:~

Numbered

Changes

not automatically supersede

all

outstanding Temporary Right

Manual

Changes.

instructions given

"Note" on Ustof

Effective

Pages

determine which Temporary Right

Manual

Changes to

remove when incorporating a

Numbered

Change.

RETENTION

FUGHT

MANUAL

PERFORMANCE

DATA

The performance data

Section V of

this

manual

provides

performance

data

for

all

aircraft

with

the

same

model designation rather than perfor-

mance data for a

Specific

serial

number

aircraft.

Therefore,

due

to serial

number changes or the incorporation

Airplane Modibtion

Kits

(AMK's),

Airplane

Accessory

Kits

(AAK's)

Service

Bulletins,

petformance

charts

may

be issued against

this

Right

Manual

which

not applicable to

the

specific

aircraft assigned to the Right

Manual.

is pennissible to relo-

cate performance data not applicable to your

speci&:

aircraft to the rear of

the manual.

Retention

relocated performance data

required

all

pages

listed

on the Ust

Effective

Pages constitute

a complete

FAA

Approved Airplane Right

Manual.

Ad-

ditionally,

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

iii

~mlAUBD[]U

Im~

111.11,

••••

INTRODUcnON

(CONT)

NOTES,

CAUTIONS,

AND

WARNINGS

Notes, Cautions, and Warnings are

used

throughout

this

manual to

focus

at-

tention on

special

conditions or procedures

follows:

Notesare

used

to highlight

specific

operating conditions

steps

ofa procedure.

Cautions are

used

call

attention to operating

proce-

dures

which,

not sbictly

observed,

may

result

dam-

age to equipment.

Warnings are

used

call

attention to operating

proce-

dureswhich, ifnotsbictIy adhered to, may result

per-

sonal

injury

loss

life.

OrnER PUBUCAll0NS

The

foHowing

a list of learjet publications referenced

this

Airplane

Right

Manual.

Such references

this

manual are made by number

and

not contain any

revision

indication.

However,

such

references are to be

un-

derstood

"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

18,000 Pounds

Installation of Conical Fan Spinner

for

TFE

731

Engines

Installation

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

Components to

Allow

Variable

Pitch

Trim

Settings at

Takeoff

Installation of

Windshield

Defog

Improvement

FAA

APPROVED

4-30-76

REISSUED

2·25-81,

CHANGE

INTRODUCTION (CONT)

AIRPlANE

MODIFICATION

KITS

(AMK)

AMK

76-3

AMK

76-7

AMK

78-13

AMK80-17

AMK83-5

AMK85-1

AMK90-3

AMK

91-2

Installation of Anti-Skid and

Nose

Steering

Interface

Electri-

cal

Box

Relocation of

Cabin

Air

Disbibution Row

Control

Valve

Installation ofSplit Essential

Bus

Elechical

System

Installation of Current Umiter

Warning

and Starter

Indica-

tor Ughts

InstaDation

Wing

Fences,

Stall

Ships

and

Boundary

Layer

Energizers

(Softflite)

(Supersedes

79-10)

Electrical Power Distribution Improvement

InstaUation

of Emergency Pressure Control

Circuit

Breaker

Replacement of

Wmdshield

Anti-ice

Thermostats I

ENGINEERING

CHANGE

RECORDS

(ECR)

ECR

1495 18,000 Pounds

T.O.G.W.

ECR

2234

Takeoff Gross Weight Increase

REID

CHANGE

NOTICES

(FCN)

FCN

89-1

Increase

Altitude

Urnitation

for

Operation

Freon

Air

Conditioning System

SERVICE

BULLETINS

(SB~

35/36-21-17

35/36-22-4

35/36-27-7

35/36-28-11

35/36-32-4

Installation

Wmdshield

Defog Improvement I

Modification

Mach

Trim

Computer

Modification

of Spoileron Computer

Assembly

Installation

of Standby

Fuel

Pump Annunciators

Replacement of

Landing

Gear

Hydraulic

Selector

Valve

FAA

APPROVED

4-30-76

RBSSUED

2-25-81,

CHANGE

10 v

FAA APPROVED 4-30-76 I-1

REISSUED 2-25-81, CHANGE 10

SECTION I — LIMITATIONS

TABLE 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