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DURING TAKEOFF
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TM-55-1510-218-MTF Maintenance Test Flight Manual Army Model C-12C C-12D and C-12F Aircraft
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DURING CLIMB (CONT) - TM-55-1510-218-MTF0060
TM 55-1510-218-MTF
PROCEDURE
TROUBLESHOOTING
REFERENCE
5. Propeller synchronization switch -
As required.
6. Yaw damp switch - As required.
7. Autofeather switch - As required.
8. Cabin pressurization - Check.
*9. Wings and nacelles - Check for fuel
E29
and oil leaks.
*10. Brake deice system - Check as fol-
lows:
a. BRAKE DEICE ON annuncia-
tor light - Check extinguished
within approximately 10 min-
utes of landing gear retraction.
b. Brake deice switch - Turn off
then on and observe that
BRAKE DEICE ON light does
not illuminate.
c. Landing gear switch - DN. Ob-
serve BRAKE DEICE ON light
illuminates.
d. Brake deice switch - Off.
e. Landing gear switch - UP.
DURING CLIMB
*1. Engine and flight instruments - B1-9,C44
Monitor. All instruments must give
proper indication with minimum
fluctuation.
*2. Engine control levers - Check for
alignment.
*3. Vertical speed indicators - Check
B2
normal operation against altimeter
as follows:
2-49

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