TM 1-1510-262-10
Monitor TGT during shutdown. If sustained combustion is observed, proceed immediately to Abort
Start procedure.
CONDITION levers -- FUEL CUTOFF.
14.
PROP levers -- FEATHER.
15.
Oxygen system -- OFF.
16.
COCKPIT LIGHTS switches -- OFF.
17.
Do not turn exterior lights off until propeller rotation has stopped.
EXTERIOR LTS switch -- OFF.
18.
IFF MODE 4 CODE switch -- HOLD as required.
19.
AVIONICS MASTER POWER switch -- OFF.
20.
MASTER SWITCH -- OFF.
21.
Key lock switch -- OFF.
22.
ESIS -- TEST then OFF.
23.
8-40. BEFORE LEAVING AIRCRAFT.
NOTE
Brakes should be released after chocks are in place (ramp conditions permitting).
1.
Wheels -- Chocked.
PARKING BRAKE -- As required.
2.
3.
Flight controls -- Locked.
STANDBY PUMP switches -- OFF.
4.
5.
Windows -- As required.
6.
Emergency exit lock -- As required.
Cabin lights -- OFF.
7.
Door light -- OFF.
8.
9.
Walk-around inspection -- Complete. Check overall condition of the aircraft. Install the right wing ASE
safety pin. Compare CMWS electronic inventory to physical inventory and note any discrepancy.
10. Aircraft forms -- Complete.
11. Aircraft -- Check secured.
SECTION III. INSTRUMENT FLIGHT
8-41. GENERAL.
This aircraft is qualiied for operation under instrument light meteorological conditions. Handling characteristics,
stability characteristics, and range are the same during instrument light conditions as when under visual light con-
ditions.
8-42. INSTRUMENT FLIGHT PROCEDURES.
Refer to FM 3-04.240, DOD FLIP, AR 95-1, and procedures described in this manual or applicable foreign regula-
tions.
