Learjet 35 - Page 292

4C-16 Developed for Training Purposes Leerjet 35/36
February 1998
CAE SimuFlite
Pressurization System
Power Source Engine bleed air: regulated vacuum jet
pump
Cabin air
Ambient air
DC power: RH DC ESS A bus
Distribution Safety valve
Automatic cabin altitude controller
Cabin altitude limiter
Outflow valve
Control Squat switches
Cabin air switch
AUTO/MAN switch
UP/DN altitude control
Cabin altitude aneroid switch
‘ Emergency pressurization valves
9,500 ft cabin altitude pressure switches
(35-107, 113 and subsequent
36-032 and subsequent)
Monitoring L/R BLEED AIR annunciators
CAB ALT annunciator
Cabin altitude warning
Cabin climb gage
Cabin altitude gage
Protection CAB PRESS CB
Safety valve
Exhaust and safety valve
Cabin altitude limiter