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ENGINE RUNUP (CONT) - TM-55-1510-218-MTF0053
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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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ENGINE RUNUP (CONT) - TM-55-1510-218-MTF0055
TM 55-1510-218-MTF
PROCEDURE
TROUBLESHOOTING
REFERENCE
ENGINE RUNUP (CONT)
*15. Rudder boost - Check as follows:
a. Rudder boost switch - ON.
b. left engine power lever
IDLE.
c. Condition levers - LO IDLE.
d. Right engine power lever - Ad-
vance until rudder boost moves
right rudder in. The rudder
boost system should activate
within the values of N1 a n d
free air temperature specified
e. Rudder boost switch - OFF.
System should deactivate, re-
Ieasing rudder pressure.
f. Repeat above procedure for op-
posite engine.
* 16. Autoignition system - Check as fol-
lows:
a. Power Ievers - Set above 22%
b. Autoignition switches (2) -
ARM.
c. Power levers - Retard.
d. lgnition annunciator lights - II -
luminated (16 to 21% torque).
*17. Primary governors - Check as fol-
F1-3
lows:
a. Power Ievers - Set 1800 RPM.
b. Propeller levers - Move aft to
detent.
2-44

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