Leerjet 35/36 Developed for Training Purposes 4C-15
February 1998
Environmental Systems
Environmental Systems Data
Pneumatic System
Power
Source
L/R engine HP and LP bleed air
DC power – DC LH/RH Main buses
Distribution Aeronca TFE731 thrust reversers
Alcohol anti-ice reservoir
(35-107, 113, and subsequent;
36-032 and subsequent)
Pressurization control system
Modulating shutoff control valve
Nacelle heat
Emergency pressurization valves
(35-107, 113, and subsequent;
36-032 and subsequent)
Bleed air manifold
Air conditioning and heating system
Windshield defog
Wing and stabilizer leading anti-ice
Control L/R modulating control valves
L/R BLEED AIR switches
Cabin air switch
510 Pressurization system
L/R 9,500 ft cabin altitude aneroid switches
L/R emergency pressurization valves
Monitor L/R BLEED AIR annunciators
Pylon/duct temperature sensors
Duct pressure switch (removed by S/B)
9,500 ft cabin altitude –
emergency pressurization
Protection RH/LH MOD VAL CB
To Next Page
Loading...
