3-24 Developed for Training Purposes Leerjet 35/36
February 1998
CAE SimuFlite
Autopilot pitch and roll axis must not be used for takeoff or
landing.
Minimum altitude for autopilot use is 200 ft AGL on approach
and 1,000 ft AGL in cruise.
Maximum lateral fuel imbalance for autopilot use is 200 lbs.
If severe turbulence encountered, use attitude hold mode with
SOFT mode engaged.
Autopilot may not be used in any axis that fails Autopilot Moni-
tor check.
Autopilot must be disengaged before switching static sources.
For VOR approach, the flaps must be lowered to 8° or more.
Drag Chute
Do not deploy:
Q
in flight
Q
at speeds in excess of 150 KIAS
Q
simultaneously with thrust reversers (if installed).
Demonstrated crosswind velocity is 20 knots. The drag chute
may not be used to supersede runway length requirements
published in the AFM.
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