Learjet 35 Learjet3 04 Preflight

Leerjet 35/36 Developed for Training Purposes 2A-1February 1998

Preflight InspectionTable of ContentsTable of ContentsPower 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 35/36February 1998

CAE SimuFlite

Power Off Inspection Exterior Walkaround

Prior to performing the Power Off checks, remove and stow thecontrols lock.

A Left NoseDefog/Alcohol Discharge Outlets . . . . . . . . . . . . . . . . . . CLEAR

Pitot Head (FC-200)/Probe (FC-530) . . . . . .REMOVE COVER/ 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 . . . . . . . . . . . . . . . . . . . . CHECK FOR 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 () denote through-flight checklist items.

Preflight Inspection Walkaround Path


Preflight Inspection

B Right NoseOxygen Bottle Supply Valve (if installed) . . . . . . . . . . . . . . ONPitot Head (FC-200)/Probe (FC-530). . . . . .REMOVE COVER/. . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLEAR

Total Temperature Probe (if installed) . . . . . . . . . . . . . CLEARStall Warning Vane. . . . . . . . . . . . . . . . . . . .FREE AND DOWN

Static Ports/Shoulder Static Port (FC-200). . . . . . . . . . . CLEARPitot Static Drain Valves. . . . . . . . . . . . . . . . . . . . . . . . . DRAIN

Pressurization Static Port. . . . . . . . . . . . . . . . . . . . . . . . CLEAR

Oxygen Discharge Disk (if installed) . . . . . CHECK IN PLACEDefog Outlet. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLEAR

Lower Fuselage Antennas/Rotating Beacon . . . . . . . . .CHECK

Wing Inspection Light (if installed) . . . . . . . . . . . . . . . .CHECK

2A-4 Developed for Training Purposes Leerjet 35/36December 2001

CAE SimuFlite

C Right Wing RootEmergency 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.



D Right Wing ForwardRight Wing Access Panels . . . . . . CHECK FOR FUEL LEAKS

Right Fuel Vent . . . . . . . . . . . . . . . . PLUG REMOVED/CLEAR

Wing Surface . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . INSPECTStandard Wing:

Vortex Generators . . . . . . . . . . . . . . . . . . . . . . . . . .CHECKCentury III Wing With Softflite:

Stall Strip/Stall Fence . . . . . . . . . . . . . . . . . . . . . . . .CHECK

Boundary Layer Energizers . . . . . . . . . . . . . . . . . . .CHECKCentury III Wing Without Softflite:

Vortex Generators . . . . . . . . . . . . . . . . . . . . . . . . . .CHECKMark IV Wing:

Stall Strip/Stall Fences . . . . . . . . . . . . . . . . . . . . . . .CHECK

Right Wing Heat Scupper . . . . . . . . . . . . . . . . . . . . . . . CLEAR

RAISBECKMARK IV WING

CENTURY III WINGWITHOUT SOFTFLITE

VORTEX GENERATORS

STALLSTRIP

STALLFENCE

STRAKESTRAKE

CENTURY III WINGWITH SOFTFLITE

STALLFENCE

STALLSTRIP

BOUNDARY LAYERENERGIZERS (BLEs)VORTEX GENERATORS

STANDARD WING

STRAKESTRAKE


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E Right Tip TankRight 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 AftAccess Panels . . . . . . . . . . . . . . . . CHECK FOR FUEL LEAKS

Aileron . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CHECK

Spoiler . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CHECK

Flap . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CHECK



G Right Nacelle/Aft LWR FuselageRight 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 completelystowed.

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). . . DRAINFuel Drains (3) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DRAIN


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H Aft Compartment/TailconeTailcone 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) . . . . . . . . . . . . . . . . . . . . . SECURECompartment Light (if installed) . . . . . . . . . . . . . . . . . . OUTDrag Chute (if installed) . . . . . . . . . CHECK FOR PROPER. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .INSTALLATION

See AFM supplement for appropriate instructions for proper drag chute installations.

Tailcone Access Door . . . . . . . . . . . . . . . . . . CLOSE/SECURE



I EmpennageRight Fuel Computer Drain Valve . . . . . . . . . . . . . . . . . DRAIN

Oxygen Bottle Supply Valve (if installed) . . . . . . . . . . . . . . ONOxygen Discharge Disk (if installed) . . . . . CHECK IN PLACERight VOR/LOC Antenna. . . . . . . . . . . . . . . . . . . . . . . .CHECK

Right ELT Antenna (if installed) . . . . . . . . . . . . . . . . . .CHECKVertical 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) . . . . . . . . . . . . . . . .CHECKLeft VOR/LOC Antenna . . . . . . . . . . . . . . . . . . . . . . . . .CHECK

Left ELT Antenna (if installed) . . . . . . . . . . . . . . . . . . .CHECKLeft Fuel Computer Drain Valve. . . . . . . . . . . . . . . . . . . DRAIN

WARNING: The vertical and horizontal stabilizer and flight control surfaces must be free of frost, snow, and ice.


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J Left NacelleFire 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



K Left Wing AftSpoiler . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CHECK

Flap . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CHECK

Aileron . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CHECK

Access Panels . . . . . . . . . . . . . . . . CHECK FOR FUEL LEAKS

L Left Tip TankJettison 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) . . . . . . . .CHECKLeft Tip Tank . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CHECK

2A-12 Developed for Training Purposes Leerjet 35/36December 2001

CAE SimuFlite

M Left Wing ForwardWing 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



Left Engine Inlet/Fan . . . . . . . . . . . . . . . . . . . . CHECK CLEAR

Cabin Door Seal . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CHECK

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.


CAE SimuFlite



Power On ChecksLanding Gear Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . DOWN

Battery Switches Both . . . . . . . . . . . . . . . . . . . . . . . . . . . ON

Fuel Quantities. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CHECK

Pitot Heat Switches . . . . . . . . . . . . . . . . . . . . . . ON/TEST/OFF

Exterior Light Switches . . . . . . . . . . . . . . . . . . . ON/TEST/OFF

Battery Switches Both. . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

Stall Warning System Test (Standard Wing) . . . . . . PERFORM

See AFM for appropriate instructions for performing the Stall Warning System Test.

Cabin InspectionBaggage . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECURE

Cabin Air Damper Control Knob/or Cabin Blower Switch . . . . . . . . . . . . . . . . . . .AS REQUIRED

Emergency Exit . . . . . . . . . . . . . . . . . . . . . . . . . AISLE CLEAR/ . . . . . . . . . . . . . . . . . .HANDLE UNOBSTRUCTED

Passenger Briefing . . . . . . . . . . . . . . . . . . . . . . . . COMPLETE


CAE SimuFlite

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Learjet 35 Learjet3 04 Preflight