Leerjet 35/36 Developed for Training Purposes 4B-19
February 1998
Electrical System
Electrical Systems Data
Distribution (cont.), Control, Monitor and Protection on following page.
Power Source Generators (28.5V DC output)
Air: 400A air max load
Ground: 320A ground max load
Main aircraft batteries (24V DC output)
Ni-cad or lead-acid
Static inverters (two or three)
110 – 130 AC output
Emergency battery(s)
Ground Power Unit (28V DC, 1,100A out-
put)
Distribution DC with battery switches in BAT 1/2 and/
or generators operating:
Battery/Battery Charging bus
LH/RH Hot Battery buses
LH/RH Generator buses
LH/RH Main buses
LH/RH Essential (A/B) buses
AC with main inverter switches in PRI/
SEC and/or auxiliary inverter switch in
ON:
LH/RH AC bus, 115V AC bus:
Spoileron
Floodlights
Flight director
Direct gyro
Vertical gyro
Radar
Yaw damper
26V AC bus:
Mach indicator
SAT TAS
RMI
NAVs
ADF
Oil pressure indicator
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