TM 1-1510-262-10
NOTE
N 1 may be increased by increasing airspeed.
Zc CONDITION lever -- LOW IDLE.
Zv Engine Cleanup checklist -- Perform if engine restart was unsuccessful.
15. POWER -- As required (after TGT peaks).
Zn ENVIRO & PNEU BLEED AIR switch -- ON.
Zm GENERATOR switch -- RESET , then ON.
18. PROP SYNC switch -- As required.
Zj Electrical equipment -- As required.
Xk CONDITION lever -- HIGH IDLE.
Xz CABIN AIR MODE SELECT switch -- As required.
Xx TCAS -- As required.
9-11. ENGINE RESTART DURING FLIGHT (USING STARTER).
Engine restarts should only be attempted below 25,000 feet. If a restart is attempted, perform the following:
The pilot should determine the reason for engine failure before attempting an airstart. Do not
attempt an airstart if N 1 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.
! CABIN AIR MODE SELECT switch -- OFF.
@ ENVIRO & PNEU BLEED AIR switch (inoperative engine) -- PNEU ONLY.
# FWD VENT BLOWER switch -- AUTO.
$ AUTO PLT POWER switch -- Off.
% Wx Radar MODE switch -- OFF.
^ POWER lever -- IDLE.
& PROP lever -- Low RPM.
* CONDITION lever -- FUEL CUTOFF.
( FIRE PULL handle -- Push in (to extinguish annunciator).
NOTE
If conditions permit, reduce power on the operative engine to obtain a TGT of 700 C or less to
reduce the possibility of exceeding TGT limit. Reduce electrical load to minimum consistent with
light conditions. False fuel low indications may be observed with the starter engaged and the
CONDITION lever in FUEL CUTOFF.
Zk ENG START switch -- START-IGNITION . Check IGN ON annunciator illuminated.
Zz CONDITION lever -- LOW IDLE.
Zx ENG START switch -- OFF after TGT peaks.
Zc Engine Cleanup checklist -- Perform if engine restart was unsuccessful.
Zv CONDITION lever -- HIGH IDLE.
Zb PROP lever -- As required.
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