Monitor TGT during shutdown. If sustained combustion is observed, proceed immediately to Abort
CONDITION levers -- FUEL CUTOFF.
Oxygen system -- OFF.
COCKPIT LIGHTS switches -- OFF.
Do not turn exterior lights off until propeller rotation has stopped.
EXTERIOR LTS switch -- OFF.
IFF MODE 4 CODE switch -- HOLD as required.
AVIONICS MASTER POWER switch -- OFF.
MASTER SWITCH -- OFF.
Key lock switch -- OFF.
ESIS -- TEST then OFF.
8-40. BEFORE LEAVING AIRCRAFT.
Brakes should be released after chocks are in place (ramp conditions permitting).
Wheels -- Chocked.
PARKING BRAKE -- As required.
Flight controls -- Locked.
STANDBY PUMP switches -- OFF.
Windows -- As required.
Emergency exit lock -- As required.
Cabin lights -- OFF.
Door light -- OFF.
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
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-
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-