Learjet 35 - Page 323

Leerjet 35/36 Developed for Training Purposes 4F-9
October 2001
Fuel System
Fuel System Data
*Recognition light in both tip tanks.
Capacities
Tips
Wings
Fuselage
Both Both Model 35 Model 36
Usable
Gallons
357 352* 374 200 379
Pounds
Kerosene
2,390 2,360* 2,508 1,340 2,542
Power Source DC power: LH & RH ESSENTIAL B buses
Engine-driven fuel pressure
Distribution Tip tanks
Wing tanks
Standby pumps
Transfer pump
Optional gravity transfer line
Engine motive flow
Fuel jettison valves
Jet or standby pump
Distribution Motive flow valve, JET PUMP switch
STANDBY PUMP switches
START/GEN switch
XFER-FILL switch: standby pumps
XFER-FILL switch: transfer valve,
crossflow valve, optional fuselage valve
Right wing pressure switch
Fuselage full float switch
FUSE VALVE OPEN/CLOSE switch
(gravity flow) (optional Learjet 35)
CROSSFLOW OPEN/CLOSE switch
FUEL JTSN switch
ENG FIRE PULL T-handle