Learjet 35 - Page 269

Leerjet 35/36 Developed for Training Purposes 4B-13
February 1998
Electrical System
DC System
DC power sources include:
Q
two 400A, 30V engine-driven generators regulated to
28.5V DC
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two 24V or 25V ni-cad or two 25V lead acid batteries
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28V external power system. Electrical buses distribute
power from these sources to the various systems requir-
ing DC power. Thermal circuit breakers between the bus
and the using system protect the aircraft electrical sys-
tem and equipment from electrical faults.
On aircraft 35-002 to 35-201, 35-205 and 36-002 to 36-040
without AMK 78-13, the DC buses include:
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Battery Charging bus
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Left and Right Battery buses
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Left and Right Main Power buses
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Left and Right Main buses
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Left and Right Generator buses
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Left and Right Essential buses.
On aircraft 35-202 to 35-204, 35-206 and subsequent, 36-
041 and subsequent, and prior aircraft with AMK 78-13, the
DC buses include:
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Battery Charging bus
Q
Left and Right Battery buses
Q
Left and Right Main Power buses
Q
Left and Right Main buses
Q
Left and Right Generator buses
Q
Left and Right Essential A buses
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Left and Right Essential B buses.