Leerjet 35/36 Developed for Training Purposes 3-55
February 1998
Limitations – U.K.
Flight Controls
Modified Control Wheel Configuration with Stick Pusher
Cutout (U.K., Canadian aircraft)
Do not operate stick pusher cutout above 0.74 M
I.
If the stick pusher cutout is engaged (PITCH SERVO DISABLE
illuminated), do not exceed 0.74 M
I (Refer to AFM Section I,
Stick Puller).
If stick puller inoperative, maximum Mach number is 0.74 M
I.
Both yaw dampers must be operative. One yaw damper must
be on and operative for all flight conditions except takeoff and
landing touchdown. For a normal landing, the following proce-
dures shall apply.
Q
The airplane shall be configured for landing at least 500 ft
AGL.
Q
On aircraft with the FC-200 autopilot, the yaw damper
shall be disengaged during the landing flare.
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