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TM-1-1510-225-MTF Army Model C-12 Aircraft Manual | Next
AUTOFEATHER switch |
TM 1-1510-225-MTF
PROCEDURE
TROUBLESHOOTING
REFERENCE
NOTE
If conditions permit, reduce power on the opera-
tive engine to obtain an ITT of 700°C or less to
reduce the possibility of exceeding ITT limit.
Reduce electrical load to minimum consistent
with flight conditions.
False fuel flow indications may be observed with
the starter engaged and the CONDITION lever in
FUEL CUTOFF.
(9) IGNITION and ENGINE
START switch - ON. Check
IGNITION ON annunciator
illuminated.
(10) CONDITION lever - LOW
IDLE.
(11) IGNITION and ENGINE
START switch - OFF, after
ITT peaks.
(12) CONDITION lever - LOW
IDLE.
(13) PROP lever - As required
(14) POWER lever - As required
(15) GEN switch - RESET, then
ON.
(16) Engine AUTO IGNITION -
As required.
(17) PROP SYN switch - As
required.
(18) Electrical equipment - As
required.
(h) Repeat step (g) for opposite
engine if required
*10. Propeller autofeathering system and
2-57
F4,14-15
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