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Electrical Charging System
General
This chapter includes inspection and maintenance
information
for
the
charging system.
For a description of the aircraft electrical and
charging
system,
manufacturer's documentation.
For alternator location on the engine, refer to Figure
13-1, "Alternator Location."
13-2
TCM-supplied
electrical
refer
to
the
airframe
FIGURE 13-1. ALTERNATOR LOCATION
Electrical Charging System
The TSIOL-550-C Permold Series engine direct
drive alternator is mounted on the right front
crankcase half. The alternator generates electrical
current for powering the aircraft electrical system
and for recharging aircraft batteries. For detailed
information about TCM alternators, refer to
"Alternator Service Instructions," Form X30531-3.
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