TM 55-1510-222-MTF
PROCEDURE
TROUBLESHOOTING
REFERENCE
7. Condition levers - HIGH IDLE.
8. Propeller levers - FEATHER.
9. AC and DC GPU’s - Disconnect as
required (check aircraft external
power and mission external power
annunciator lights extinguished).
10. Propeller levers - Retard to feather
detent (low RPM).
11. Power levers - GROUND FINE.
12. Aircraft inverter switches - ON.
Check #1 INVERTER and #2 IN-
VERTER annunciator lights extin-
guished.
E2
C36,37
13. Generator switches - RESET, then
ON.
14. Strobe beacon lights switch - DAY
or NIGHT as required.
BEFORE TAXIING
1. Brake deice - As required. To acti-
vate the brake deice system pro-
ceed as follows:
a. Bleed air valves - OPEN.
b. Brake deice switch - DEICE.
Check BRAKE DEICE ON ad-
visory annunciator light illumi-
nated.
2. Cabin air mode and temperature
switches - Set.
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