TM 1-1510-224-MTF
PROCEDURE
TROUBLESHOOTING
REFERENCE
(e)
PROP
lever
(engine
to
be
feathered) - FEATHER. Time to
feather must not exceed 10 seconds
from 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.
WARNING
Aristocrats 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.
2-73
