Yaw damp - As required.
8-51. AFTER LANDING.
Complete the following procedures after the
aircraft has cleared the runway:
CONDITION levers - As required.
Engine autoignition switch - OFF.
Ice & rain switches - OFF.
Flaps - UP.
Transponder - As required.
Radar - As required.
Lights - As required.
Mission control panel - Set.
8-52. ENGINE SHUTDOWN.
To prevent sustained loads on rudder shock
links, the aircraft should be parked with the
nose gear centered.
Brake deice - OFF.
Parking brake - Set.
Landing/taxi lights - OFF.
Cabin temperature mode selector switch -
Autofeather switch - OFF.
Vent and aft vent blower switches -
INS - OFF.
Mission equipment - OFF, as required.
Inverter switches - OFF.
Battery condition - Check as required.
TGT - Check. TGT must be 660°C or below
for one minute prior to shutdown.
Monitor TGT during shutdown. If sustained
combustion is observed, proceed immediately
to ABORT START procedure.
8-22 Change 4
Propeller levers - FEATHER.
CONDITION levers - FUEL CUTOFF.
Do not turn exterior lights off until propellers
rotation has stopped.
Exterior lights - OFF.
Master panel lights switch - OFF.
Avionics master switch - Off.
Master switch - OFF. -
Keylock switch - OFF.
Oxygen system - OFF.
8-53. BEFORE LEAVING AIRCRAFT.
Wheels - Chocked.
Parking brake - As required.
Brakes should be released after chocks are in
place (ramp conditions permitting).
Flight controls - Locked.
Overhead flood lights - Off.
Standby fuel pump switches - OFF.
Transponder - OFF.
Mode 4 - As required.
KY-28/58 - Zeroize as required.
Emergency exit lock - As required.
Aft cabin light - OFF.
Door light - OFF.
If strong winds are anticipated while the
aircraft is unattended, the propellers shall be
secured to prevent their windmilling with zero
engine oil pressure.
12. Walk-around inspection - Complete. Conduct
a thorough walk-around inspection. Checking
for damage, fluid leaks. and levels. Check that
covers, tiedowns. restraints.