Learjet 35 - Page 10

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). . . . . .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 (ç) denote
through-flight checklist items.
Preflight Inspection Walkaround Path