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Learjet 35 - Page 312

Learjet 35
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4E-12 Developed for Training Purposes Leerjet 35/36
February 1998
CAE SimuFlite
Spoilers
Flaps
Stall Warning
Power Source Engine-driven hydraulic pump
Control DC RH ESSENTIAL B bus
Spoileron computer – RH 115V AC bus
Aileron augmentation – flap 25° switch
Flashing spoiler light – flap 13° switch
Monitor AUG AIL annunciator – split condition
SPOILER annunciator:
Steady – not locked down
Flashing – flaps and spoilers
extended
Power Source Electrically controlled,
hydraulically operated
Control Flap switch
Monitor Flap indicator
Protection Mechanical flap interconnect
Power Source Left stall warning –
DC LH HOT BATTERY bus
Right stall warning –
DC RH HOT BATTERY bus
Control Mach overspeed
Nudger (530 autopilot)
Nudger monitor (530 autopilot)
Puller (left side only)
Pusher
Stick shaker
Monitor L/R stall – annunciator lights
L/R stall – stall margin indicators

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