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.