TM 1-1510-224-10
9-9. ENGINE RESTART DURING FLIGHT (NO
STARTER ASSIST).
CAUTION
This procedure should be conducted
only
during
an
emergency
and
should
not
be
practiced
or
demonstrated. This procedure will
cause damage to the engine hot
section.
CAUTION
The
pilot
should
determine
the
reason for engine failure before
attempting an airstart. Do not
attempt an airstart if N, indicates
zero. Do not attempt engine airstarts
above
25,000
ft.
As
engine
accelerates to idle speed, it may
become
necessary
to
move
the
condition lever into FUEL CUTOFF in
order to avoid an over temperature
condition.
(1)
POWER lever - IDLE.
(2)
PROP lever - HIGH RPM.
(3)
CONDITION lever - FUEL CUTOFF.
(4)
CABIN AIR MODE SELECT switch - As
required.
(5)
FIRE PULL handle - Push (PUSH TO
EXTINGUISH annunciator extinguished).
(6)
Engine anti-ice - Off.
(7)
GENERATOR switch (inoperative engine)
- OFF.
8.
Airspeed
-
As
required
(140
kn6ts
propeller windmilling, 190 knots propeller
feathered).
9.
Altitude - Below 25,000 feet.
10.
Engine cleanup - Perform if engine restart
is unsuccessful.
(11)
Engine N, - Monitor (10% minimum,
propeller feathered).
NOTE
N, may be increased by increasing
airspeed.
(12)
AUTO IGNITION switch - ARM.
(13)
CONDITION lever - LOW IDLE.
14.
Power - As required (after TGT peaks).
(15)
GENERATOR switch - RESET, then ON.
16.
PROP SYNC switch - As required.
17
Electrical equipment - As required.
(18)
CONDITION lever - HIGH IDLE.
(19)
CABIN AIR MODE SELECT switch - As
required.
9-10. ENGINE RESTART DURING FLIGHT (USING
STARTER).
Engine restarts should only be attempted below
25,000 feet. If a restart is attempted, perform the
following:
CAUTION
The
pilot
should
determine
the
reason for engine failure before
attempting an airstart. Do not
attempt an airstart if N1 indicates
zero.
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)
FWD VENT BLOWER switch - AUTO.
(3)
AUTO PLT POWER switch - Off.
WARNING
Airstarts using the starter assist
procedures will cause the momentary
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.
(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.
9-4
