Leerjet 35/36 Developed for Training Purposes 4E-13
February 1998
Flight Controls
Pitch Trim – Horizontal Stabilizer
Power Source Primary Trim – power battery
Control power DC LH ESSENTIAL
Secondary Trim –
Power and control DC
ESSENTIAL B bus
Control Primary:
L/R yoke switch
Trim switch (pedestal)
PRI-OFF-SEC switch
L/R wheel master (cutout)
L yoke overrides R yoke
Two speed (530 autopilot only)
Flaps up – slow
Flaps 3° – fast
Mach trim computer
above 0.69 M
I
RH 115V AC bus
Secondary:
Secondary trim switch (pedestal)
Trim switch (pedestal)
PRI-OFF-SEC switch
Autopilot
Wheel master cutout (530 autopilot)
Monitor TO TRIM annunciator
Trim indicator
530 autopilot
TRIM OV SPEED annunciator
Audio trim in motion “clicker”
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