TM 1-1510-224-10
8-36. ENGINE SHUTDOWN.
NOTE
To prevent sustained loads on rudder
shock links, the aircraft should be
parked with the nose gear centered.
1.
PARKING BRAKE - Set.
2.
LANDING/TAXI LIGHTS switches - OFF.
(3)
INS - OFF.
4.
BUS CROSS TIE switch - OFF.
5.
CABIN AIR MODE switch - OFF.
6.
FWD and AFT VENT BLOWER switches
- AUTO.
7.
AUTOFEATHER switch - OFF.
8.
Inverter switches (4) - Off.
9.
AUTO PLT POWER switch - Off.
10.
# 1 and # 2 EFIS POWER switches - Off.
11.
BRAKE deice - Off.
12.
Battery condition - Check.
13.
TGT - Check stabilized for 1 minute prior
to shutdown.
14.
POWER levers - Flight IDLE.
15.
PROP levers - FEATHER.
CAUTION
Monitor TGT during shutdown. If
sustained combustion is observed,
proceed immediately to Abort Start
procedure.
16.
CONDITION levers - FUEL CUTOFF.
17.
Oxygen system - OFF.
WARNING
Do not turn exterior lights off until
propeller rotation has stopped.
18.
COCKPIT LIGHTS switches - Off.
19.
AVIONICS MASTER POWER switch -
Off.
20.
EXTERIOR LTS - Off.
21.
MASTER SWITCH - OFF.
22.
Keylock switch - OFF.
8-37. BEFORE LEAVING AIRCRAFT.
NOTE
Brakes should be released after
chocks are in place (ramp conditions
permitting).
1.
Wheels - Chocked.
2.
PARKING BRAKE - As required.
3.
Flight controls - Locked.
4.
STANDBY PUMP switches - Off.
5.
COMSEC - Zeroize as required.
6.
Windows - As required.
7.
Emergency exit lock - As required.
8.
Aft cabin lights - OFF.
9.
Door light - OFF.
10.
Walk-around inspection - Complete.
11.
Aircraft forms - Complete.
12.
Aircraft - Check secured.
8-25
