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 TM 1-1510-223-MTF
PROCEDURE
TROUBLESHOOTING
REFERENCE
LOW SPEED SYSTEMS CHECK (CONT)
windmilling at 1700 RPM to no rotation in
the feathered position.
f. Engine cleanup.
(1) CONDITION lever - FUEL CUTOFF.
(2) AUTO IGNITION switch -Off.
(3) AUTOFEATHER switch -OFF.
(4) GENERATOR switch - OFF.
(5) PROP SYN switch - OFF.
g. Engine restart.
Airstarts using the starter assist procedures will
momentarily cause the loss of all electronic flight
instrument system (EFIS) data. The engine restart
during flight (no starter assist procedure), or
turning EFIS power off prior to a starter assisted
restart, should normally be performed.
CAUTION
Do not attempt engine airstarts above 25,000 feet.
During engine acceleration to idle speed, it may
become necessary to move the CONDITION lever
into FUEL CUTOFF in order to avoid an over
temperature condition.
(1) CABIN AIR MODE SELECT switch -
OFF.
2-68
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