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Home > Aviation Maintenance and Training Volume 2 > > Double inverter failure - P-12600156
Single inverter failure - P-12600155
Cockpit lighting failure - P-12600157

Emergency Flight Procedures - index
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T-45C TS, ADV & IUT EMFP-08
Electrical and Indicator Emergency Procedures
(2) AC INV caution light illuminates
(3) Loss of all nonessential AC equipment
b.
Procedures - See NATOPS
Sg 1, fr 9
AC Reset Switch
2.
Double inverter failure 1.8.1.3.1.3.2
a.
Indications
(1) MASTER ALERT light flashes and caution
tone sounds
(2) AC INV caution light illuminates
(3) Loss of all AC equipment
b.
Procedures: comply with AC inverter failure
procedures
LESSON NOTES
Give an example of what could happen if the reset switch is
held in place.
C.
Total electrical failure 1.8.1.3.1.4.1, 1.8.1.3.1.4.2
1.
Indications
a.
All electrically controlled flight instruments
cease to function
b.
Loss of all aircraft lights (internal and external)
c.
Loss of flaps/slats, stabilator trim, rudder trim,
yaw damper, and aileron trim
d.
Loss of communication systems and navigation
systems
Original (9-98)
Page 8-7






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