TM 1-1510-224-CL
INS
ADF
#1 rate of turn
#2 rate of turn
Air data computer
Under these conditions, power must be governed by indications
of N1 and TGT gages. Perform the following:
1.
N1 and TGT indications - Check.
2.
Other engine Instruments - Monitor.
CIRCUIT BREAKER TRIPPED
1.
Bus feeder breaker tripped - Do not reset.
2.
Nonessential circuit - Do not reset
(3.) Essential circuit - Reset once.
BATTERY CHARGE ANNUNCIATOR ILLUMINATED
(1.) Battery ammeter - Check, note indication, and monitor
for Increasing load. If load continues to Increase, turn
battery switch OFF.
(2.) BATTERY switch - OFF.
(3.) BATTERY switch (landing gear/flap extension only) -
ON.
AVIONICS MASTER POWER SWITCH FAILURE
(1.) AVIONICS MASTER CONTR circuit breaker- Pull.
BAT FEED FAULT ANNUNCIATOR ILLUMINATED
(1.) BATTERY switch - RESET, then ON.
EMERGENCY DESCENT
1.
POWER levers - IDLE.
2.
PROP levers - HIGH RPM.
3.
Flaps - APPROACH.
4.
Gear- DN.
5.
Airspeed - 179 KIAS (0.472 Mach) maximum.
E-11
