Learjet 35 - Page 311

Leerjet 35/36 Developed for Training Purposes 4E-11
February 1998
Flight Controls
Flight Controls Data
Basic Flight Controls
Power Source Trim – DC LH ESSENTIAL B bus
Autopilot – DC LH ESSENTIAL B bus
Dual yaw damper computers –
115V AC actuator and
DC LH ESSENTIAL B bus
Control Trim – yoke/pedestal switch
Autopilot – yoke switch
Dual yaw dampers – pedestal buttons
Monitor Trim – pedestal trim gages
Autopilot – autopilot force gages
Dual yaw dampers – pedestal lights
and force indicators
Protection Left CB Panel
Pitch (PITCH) – Primary STAB ACT
Roll (ROLL) – Aileron TRIM TAB
Yaw (YAW) – Rudder TRIM TAB
Left stall warning (L STALL WRN)
Primary yaw damper (PRI YAW
DAMPER)
Mach trim (MACH TRIM)
Right CB Panel
Tab and flap position (TAB & FLAP
POSN)
Spoilers (SPOILER)
Flaps (FLAPS)
Test system (TEST SYSTEM)
Secondary pitch trim (SEC STAB
ACT)
Right stall warning (R STALL WRN)
Secondary yaw damper (SEC YAW
DAMP)