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LOW SPEED SYSTEMS CHECK (CONT) - TM-55-1510-218-MTF0073
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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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LOW SPEED SYSTEMS CHECK (CONT) - TM-55-1510-218-MTF0075
TM 55-1510-218-MTF
PROCEDURE
TROUBLESHOOTING
REFERENCE
LOW SPEED SYSTEMS CHECK (CONT)
b. Autofeather switch - ARM.
c. Airspeed - 103 KIAS.
d. Propeller levers - Set 2000
RPM.
e. Condition lever (engine to be
feathered) - IDLE CUTOFF.
*f. Record the time from fuel cut-
off until propeller rotation
stops. Autofeather time is a
function of oil temperature as
shown in figure 8. (Propeller is
considered to be feathered
when the blades are individual-
ly visible to the human eye, but
the propeller is still rotating.)
For proper autofeather operation propeller
must stop completely.
g. Engine cleanup.
(1) Condition lever - FUEL
CUTOFF.
(2) Engine autoignition switch
- OFF.
(3) Autofeather switch - OFF.
(4) Generator switch - OFF.
(5) Propeller synchronization
switch - OFF.
h. Engine restart.
2-64

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