4B-20 Developed for Training Purposes Leerjet 35/36
February 1998
CAE SimuFlite
Electrical Systems Data (cont.)
Distribution
(continued)
Emergency battery 1 operating:
Standby gyro
Landing gear
Flap solenoid
Landing gear lights
Emergency battery 2 operating:
Optional equipment
Control Starter/generator switches
Main aircraft battery switches
Main inverter switches
Auxiliary bus switches (if installed)
Emergency power switch(es)
Monitor L/R Gen annunciators
L/R DC ammeters
DC voltmeter
Battery temperature indicator (if installed)
BAT 140/BAT 160 annunciators
Starter engaged lights (if installed)
PRI/SEC INV annunciators
AUX INV annunciator (if installed)
AC voltmeter
EMER PWR or EMER PWR 1/
EMER PWR 2 annunciators
CUR LIM annunciator (if installed)
Current limiter functional test lights
(if installed)
Protection Circuit breakers
Current limiters
Generator control unit (GCU)
Overload control sensors
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