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Engine cleanup - TM-1-1510-223-MTF0080
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TM-1-1510-223-MTF Maintenance Test Flight Manual Army Model RC-12
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Propeller autofeathering system and propeller unfeathering
TM 1-1510-223-MTF
PROCEDURE
TROUBLESHOOTING
REFERENCE
(2) FWD VENT BLOWER switch- AUTO.
(3) AUTO PLT POWER switch -Off.
(4) EFIS POWER switches (2) -OFF (if
conditions permit).
NOTE
If EFIS power is turned off, aircraft attitude should
be maintained by using outside visual references
or the air driven standby attitude indicator and
turn-and-slip indicator.
(5) Radar - SBY or OFF.
(6) POWER lever - IDLE.
(7) PROP lever - Low RPM.
(8) CONDITION lever - FUEL CUTOFF.
(9) FIRE PULL handle - Push in (to
extinguish annunciator).
NOTE
If conditions permit, reduce power on the operative
engine to obtain a TGT of 700 or less to reduce
C
the possibility of exceeding TGT 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.
(10)
ENG  START  switch  -START-
IGNITION.
Check  IGN  ON
annunciator illuminated.
2-69

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