Learjet 35 - Page 20

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