Learjet 35 User manual

Learjet 35/36
Cockpit Reference Handbook
FEBRUARY 2007

Notice:This Learjet 35/36 Cockpit Reference Handbook is to be used for
aircraft familiarization and training purposes only. It is not to be used as,
nor considered a substitute for, the manufacturer’s Pilot or Maintenance
Manuals.
Copyright © 2007, CAE SimuFlite, Inc.
All rights reserved.
Excerpted materials used in this publication
have been reproduced with permission
of Learjet, Inc.
Printed in the United States of America.

Learjet 35/36 Developed for Training Purposes 1-1
February 2004
Introduction
Welcome to CAE SimuFlite!
Our goal is a basic one: to enhance your safety, proficiency
and professionalism within the aviation community. All of us
at CAE SimuFlite know that the success of our company
depends upon our commitment to your needs. We strive for
excellence by focusing on our service to you.
We urge you to participate actively in all training activities.
Through your involvement, interaction, and practice, the full
value of your training will be transferred to the operational
environment. As you apply the techniques presented
through CAE SimuFlite training, they will become “second
nature” to you.
Thank you for choosing CAE SimuFlite. We recognize that
you have a choice of training sources. We trust you will find
us committed to providing responsive, service-oriented
training of the highest quality.
Our best wishes are with you for a most successful and
rewarding training experience.
The Staff of CAE SimuFlite

1-2 Developed for Training Purposes Learjet 35/36
February 2004
CAE SimuFlite

Learjet 35/36 Developed for Training Purposes 1-3
February 2004
Introduction
Introduction
CAE SimuFlite created this reference handbook for cockpit use.
It is an abbreviated version of the CAE SimuFlite Technical
Manual and includes international flight planning information.
Please refer to the front of each chapter for a table of contents.
The Procedures chapter contains three elements: Preflight
Inspection, a sample Standard Operating Procedure (SOP),
and Maneuvers.
The Limitations chapter contains general, operational, and air-
craft systems limitations.
The alphabetically arranged Systems chapter includes key
data on particular systems and relevant color schematics.
The Flight Planning chapter includes maximum allowable
takeoff and landing weight flow charts and a sample weight and
balance form. International flight planning information includes
a checklist, a glossary of frequently used international flight
operation terms, and sample flight plan forms (ICAO and FAA)
with completion instructions.
The Servicing chapter contains servicing specifications and
checklists for fueling, defueling, and other servicing procedures.
The Emergency Information chapter provides basic first aid
instructions.
Information in the Conversion Tables chapter may facilitate
your flight planning and servicing computations.

1-4 Developed for Training Purposes Learjet 35/36
February 2004
CAE SimuFlite

Leerjet 35/36 Developed for Training Purposes 2-1
February 2004
Operating Procedures
This chapter contains three sections: Preflight Inspection, a
sample Standard Operating Procedure (SOP), and Maneuvers.
Although these procedures are addressed individually, their
smooth integration is critical to ensuring safe, efficient opera-
tions.
Preflight Inspection contains an abbreviated checklist for the
exterior inspection as well as preflight cockpit and cabin
checks.
Standard Operating Procedures details Pilot Flying/Pilot
Monitoring callouts and verbal or physical responses.
Maneuvers contains pictorial representations of specific
maneuvers.

2-2 Developed for Training Purposes Leerjet 35/36
February 1998
CAE SimuFlite

Leerjet 35/36 Developed for Training Purposes 2A-1
February 1998
Preflight Inspection
Table of ContentsTable of Contents
Power Off Inspection – Exterior Walkaround . . . . . . . . 2A-2
Left Nose. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2A-2
Right Nose . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2A-3
Right Wing Root . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2A-4
Right Wing – Forward. . . . . . . . . . . . . . . . . . . . . . . . . . . 2A-5
Right Tip Tank. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2A-6
Right Wing – Aft . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2A-6
Right Nacelle – Aft LWR Fuselage . . . . . . . . . . . . . . . . . 2A-7
Aft Compartment/Tailcone . . . . . . . . . . . . . . . . . . . . . . . 2A-8
Empennage. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2A-9
Left Nacelle. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2A-10
Left Wing – Aft . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2A-11
Left Tip Tank. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2A-11
Left Wing – Forward . . . . . . . . . . . . . . . . . . . . . . . . . . . 2A-12
Power On Checks . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2A-15
Cabin Inspection . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2A-15

2A-2 Developed for Training Purposes Leerjet 35/36
February 1998
CAE SimuFlite
Power Off Inspection –
Exterior Walkaround
Prior to performing the Power Off checks, remove and stow the
controls lock.
A Left Nose
Defog/Alcohol Discharge Outlets . . . . . . . . . . . . . . . . . . CLEAR
Pitot Head (FC-200)/Probe (FC-530). . . . . .REMOVECOVER/
CLEAR
Stall Warning Vane . . . . . . . . . . . . . . . . . . .FREE AND DOWN
Static Ports/Shoulder Static Port (FC-200). . . . . . . . . . CLEAR
Pitot/Static/Shoulder Static Drain Valves . . . . . . . . . . . . DRAIN
Nose Gear/Wheel Well . . . . . . . . . . . . . . . . . . . . CHECKFOR
HYDRAULIC LEAKS
Normal Operations Strut Extension . . . . . 2.5 TO 3.5 INCHES
Doors . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECURED
Nose Wheel/Tire . . . . . . . . . . . . . . . . . . .CHECK CONDITION
Chine 3/4 inch minimum from ground.
Tire pressure between 104 and 114 PSI (loaded),
105 ± 5 PSI (unloaded).
Nose Gear Uplock . . . . . . . . . . . . . . . . . . .CHECK FORWARD
Alcohol Discharge Port . . . . . . . . . . . . . . . . . . . . . . . . .CLEAR
Radome/Erosion Shoe/Static Discharge Tapes. . . . . . .CHECK
NOTE: Procedures marked with this symbol (ç) denote
through-flight checklist items.
Preflight Inspection Walkaround Path

Leerjet 35/36 Developed for Training Purposes 2A-3
February 1998
Preflight Inspection
B Right Nose
Oxygen Bottle Supply Valve (if installed) . . . . . . . . . . . . . . ON
Pitot Head (FC-200)/Probe (FC-530). . . . . .REMOVE COVER/
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLEAR
Total Temperature Probe (if installed) . . . . . . . . . . . . . CLEAR
Stall Warning Vane. . . . . . . . . . . . . . . . . . . .FREE AND DOWN
Static Ports/Shoulder Static Port (FC-200). . . . . . . . . . . CLEAR
Pitot Static Drain Valves. . . . . . . . . . . . . . . . . . . . . . . . . DRAIN
Pressurization Static Port. . . . . . . . . . . . . . . . . . . . . . . . CLEAR
Oxygen Discharge Disk (if installed) . . . . . CHECK IN PLACE
Defog Outlet. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLEAR
Lower Fuselage Antennas/Rotating Beacon . . . . . . . . .CHECK
Wing Inspection Light (if installed) . . . . . . . . . . . . . . . .CHECK

2A-4 Developed for Training Purposes Leerjet 35/36
December 2001
CAE SimuFlite
C Right Wing Root
Emergency Exit . . . . . . . . . . . . . . . . . . . . . . .CHECK SECURE
Upper Fuselage Antennas/Rotating Beacon . . . . . . . . .CHECK
Right Engine Inlet/Fan . . . . . . . . . . . . . . . . . . . CHECK/CLEAR
Fuel Drains (5). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DRAIN
Right Main Gear/Wheel Well . . . . . . . . . . . . . . . . CHECK FOR
HYDRAULIC LEAKS
Normal Operations Strut Extension . . . . . 2.5 to 3.5 INCHES
Right Main Gear Landing Light . . . . . . . . . . . . . . . . . . .CHECK
Right Main Gear Wheels/Brakes/Tires . . . . . . . . . . . . .CHECK
Loaded Tire Pressures:
17,000 lbs MTOGW . . . . . . . . . . . . . . . . . . 146 TO 156 PSI
18,000 lbs MTOGW . . . . . . . . . . . . . . . . . . 157 TO 167 PSI
18,300 lbs MTOGW . . . . . . . . . . . . . . . . . . 161 TO 171 PSI
WARNING: (1) If fan is windmilling, stop by pressing on fan
spinner. Do not attempt to stop windmilling by grabbing
blades. (2) The wing, flight control surfaces and engine inlet
must be free of frost, snow, and ice.

Leerjet 35/36 Developed for Training Purposes 2A-5
February 1998
Preflight Inspection
D Right Wing – Forward
Right Wing Access Panels . . . . . . CHECK FOR FUEL LEAKS
Right Fuel Vent . . . . . . . . . . . . . . . . PLUG REMOVED/CLEAR
Wing Surface . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . INSPECT
Standard Wing:
Vortex Generators . . . . . . . . . . . . . . . . . . . . . . . . . .CHECK
Century III Wing With Softflite:
Stall Strip/Stall Fence . . . . . . . . . . . . . . . . . . . . . . . .CHECK
Boundary Layer Energizers . . . . . . . . . . . . . . . . . . .CHECK
Century III Wing Without Softflite:
Vortex Generators . . . . . . . . . . . . . . . . . . . . . . . . . .CHECK
Mark IV Wing:
Stall Strip/Stall Fences . . . . . . . . . . . . . . . . . . . . . . .CHECK
Right Wing Heat Scupper . . . . . . . . . . . . . . . . . . . . . . . CLEAR
RAISBECK
MARK IV WING
CENTURY III WING
WITHOUT SOFTFLITE
VORTEX GENERATORS
STALL
STRIP
STALL
FENCE STRAKE
STRAKE
CENTURY III WING
WITH SOFTFLITE
STALL
FENCE
STALL
STRIP
BOUNDARY LAYER
ENERGIZERS (BLEs)
VORTEX GENERATORS
STANDARD WING
STRAKESTRAKE

2A-6 Developed for Training Purposes Leerjet 35/36
February 2004
CAE SimuFlite
E Right Tip Tank
Right Tip Tank . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CHECK
Recognition Light. . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CHECK
Sump Drain Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DRAIN
Fuel Cap . . . . . . . . . . . . . . . . . . . . . . . . CONDITION/SECURE
Navigation/Strobe Lights . . . . . . . . . . . . . . . . . . . . . . . .CHECK
Fin/Static Discharge Wicks (2). . . . . . . . . . . . . . . . . . . .CHECK
Jettison Tube . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CHECK
F Right Wing – Aft
Access Panels . . . . . . . . . . . . . . . . CHECK FOR FUEL LEAKS
Aileron . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CHECK
Spoiler . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CHECK
Flap . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CHECK

Leerjet 35/36 Developed for Training Purposes 2A-7
February 1998
Preflight Inspection
G Right Nacelle/Aft LWR Fuselage
Right Engine Oil. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CHECK
Oil Tank/Filler Cap/Access Door . . . . . . . . . .CHECK SECURE
Engine Oil Bypass Valve Indicator. . . . . . . . . . . . CHECK NOT
. . . . . . . . . . . . . . . . . . . . . . . . . . . .EXTENDED
Engine Turbine Exhaust Area . . . . . . . . . . . . . . . . . . . . CLEAR
Thrust Reverser . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CHECK
Aeronca – Check condition; check blocker doors completely
stowed.
Dee Howard – Check condition of doors, hinges, strike
plates; remove safety pins and flags.
Engine Fuel Bypass Valve Indicator . . . . . . . . . . . . . . .CHECK
Fuel Vent Drain Valve . . . . . . . . . . . . . . COMPLETELY DRAIN
Transfer Line Drain Valve (if FUS VALVE installed). . . DRAIN
Fuel Drains (3) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DRAIN

2A-8 Developed for Training Purposes Leerjet 35/36
February 2004
CAE SimuFlite
H Aft Compartment/Tailcone
Tailcone Access Door . . . . . . . . . . . . . . . . . . . . . . . . . . . OPEN
Tailcone Interior . . . . . . . . . . . . . . . . . . . . . . . . . . . . . INSPECT
Check for fluid leaks, security and condition of installed
equipment.
Batteries . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CHECK
Hydraulic Accumulator . . . . . . . . . . . . . . . . . . .750 PSI (MIN)
Hydraulic Reservoir Sight Gage . . . . . . . . . . . . . . . . .CHECK
Fire Extinguisher Bottles. . . . . . . . . . . . CHECK PRESSURE
(600 PSI normal/
500 PSI minimum)
Current Limiters . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CHECK
Compressor Motor Belt. . . . . . . . . . . . . . . . . . . . . . . .CHECK
Dee Howard Thrust Reverser Accumulator . . . . . . .CHECK
. . . . . . . . . . . .. . . . . . . . . . . . . . . . . . . . . . . . . . .PRESSURE
Spare Tire (if installed) . . . . . . . . . . . . . . . . . . . . . SECURE
Compartment Light (if installed) . . . . . . . . . . . . . . . . . . OUT
Drag Chute (if installed) . . . . . . . . . CHECK FOR PROPER
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .INSTALLATION
See AFM supplement for appropriate instructions for proper
drag chute installations.
Tailcone Access Door . . . . . . . . . . . . . . . . . . CLOSE/SECURE

Leerjet 35/36 Developed for Training Purposes 2A-9
February 2004
Preflight Inspection
I Empennage
Right Fuel Computer Drain Valve . . . . . . . . . . . . . . . . . DRAIN
Oxygen Bottle Supply Valve (if installed) . . . . . . . . . . . . . . ON
Oxygen Discharge Disk (if installed) . . . . . CHECK IN PLACE
Right VOR/LOC Antenna. . . . . . . . . . . . . . . . . . . . . . . .CHECK
Right ELT Antenna (if installed) . . . . . . . . . . . . . . . . . .CHECK
Vertical Stab/Rudder/Horizontal Stab/Elevator. . . . . . . .CHECK
Drain holes clear
Rudder for Freedom of Movement
Static Discharge Wicks
(6 on elevators, 1 above NAV light,
and 1 on ventral fin). . . . . . . . . . . . . . . . . . . . . . . . . . . .CHECK
Vertical Fin Navigation/Strobe Lights . . . . . . . . . . . . . . .CHECK
VLF H-Field Antenna (if installed) . . . . . . . . . . . . . . . .CHECK
Left VOR/LOC Antenna . . . . . . . . . . . . . . . . . . . . . . . . .CHECK
Left ELT Antenna (if installed) . . . . . . . . . . . . . . . . . . .CHECK
Left Fuel Computer Drain Valve. . . . . . . . . . . . . . . . . . . DRAIN
WARNING: The vertical and horizontal stabilizer and flight
control surfaces must be free of frost, snow, and ice.

2A-10 Developed for Training Purposes Leerjet 35/36
February 1998
CAE SimuFlite
J Left Nacelle
Fire Extinguisher Disks . . . . . . . . . . . . . . . . . . . . . . . IN PLACE
Engine Oil Bypass Valve Indicator. . . . . . . . . . . . CHECK NOT
. . . . . . . . . . . . . . . . . . . . . . . . . .EXTENDED
Engine Turbine Exhaust Area . . . . . . . . . . . . . . . . . . . . CLEAR
Thrust Reverser. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CHECK
Aeronca – Check condition; check blocker doors completely
stowed.
Dee Howard – Check condition of doors, hinges, strike
plates; remove safety pins and flags.
Engine Fuel Bypass Valve Indicator . . . . . . . NOT EXTENDED
Left Engine Oil . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CHECK
Oil Tank Filler Cap/Access Door . . . . . . . . . .CHECK SECURE

Leerjet 35/36 Developed for Training Purposes 2A-11
February 2004
Preflight Inspection
K Left Wing – Aft
Spoiler . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CHECK
Flap . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CHECK
Aileron . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CHECK
Access Panels . . . . . . . . . . . . . . . . CHECK FOR FUEL LEAKS
L Left Tip Tank
Jettison Tube . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CHECK
Fin/Static Discharge Wicks (2). . . . . . . . . . . . . . . . . . . .CHECK
Navigation/Strobe Lights . . . . . . . . . . . . . . . . . . . . . . . .CHECK
Fuel Cap . . . . . . . . . . . . . . . . . . . . . . . . CONDITION/SECURE
Sump Drain Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DRAIN
Erosion Shoe/Recognition Light (if installed) . . . . . . . .CHECK
Left Tip Tank . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CHECK

2A-12 Developed for Training Purposes Leerjet 35/36
December 2001
CAE SimuFlite
M Left Wing – Forward
Wing Surface . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . INSPECT
Standard Wing:
Vortex Generators . . . . . . . . . . . . . . . . . . . . . . . . . .CHECK
Softflite:
Stall Strip/Stall Fence . . . . . . . . . . . . . . . . . . . . . . . .CHECK
Boundary Layer Energizers . . . . . . . . . . . . . . . . . . .CHECK
Without Softflite:
Vortex Generators . . . . . . . . . . . . . . . . . . . . . . . . . .CHECK
Mark IV Wing:
Stall Strip/Stall Fences . . . . . . . . . . . . . . . . . . . . . . .CHECK
Left Wing Heat Scupper. . . . . . . . . . . . . . . . . . . . . . . . . CLEAR
Left Wing Access Panels. . . . . . . . . . . . . CHECK FOR LEAKS
Left Fuel Vent. . . . . . . . . . . . .REMOVE PLUG/CHECK CLEAR
Left Main Gear/Wheel Well . . . . . . . . . . . CHECK FOR LEAKS
Normal Operations Strut Extension . . . . . 2.5 to 3.5 INCHES
Left Main Gear Landing Light . . . . . . . . . . . . . . . . . . . .CHECK
Left Main Gear Wheels/Brakes/Tires. . . . . . . . . . . . . . .CHECK
Unloaded Tire Pressures:
17,000 lbs MTOGW . . . . . . . . . . . . . . . . . . 146 TO 156 PSI
18,000 lbs MTOGW . . . . . . . . . . . . . . . . . . 157 TO 167 PSI
18,300 lbs MTOGW . . . . . . . . . . . . . . . . . . 161 TO 171 PSI