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 TM 1-1510-223-MTF
PROCEDURE
TROUBLESHOOTING
REFERENCE
when the blades are individually
visible to the human eye, but the
propeller is still rotating.) Time to
feather shall not exceed 10
seconds.
NOTE
For proper autofeather operation, propeller must
stop completely.
g. 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.
h. 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.
2-71
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