Kodiak 100 Series - After Landing; Engine Shutdown and Airplane Securing

Pilot’s Operating Handbook
4-15
DO NOT USE FOR FLIGHT OPERATIONS
Section 4
NORMAL PROCEDURES
100 SERIES
Procedures
AFTER LANDING
After Landing
1. Wing Flaps ................................................................................................. UP
2. Fuel Condition Lever......................................................................LOW IDLE
3. Auxiliary Fuel Pump
.................................................................................OFF
4. Strobe Lights............................................................................................OFF
5. Landing and Taxi Lights
........................................................ AS REQUIRED
6. Pitot Heat (L&R).......................................................................................OFF
ENGINE SHUTDOWN AND AIRPLANE SECURING
Shutdown and Securing
1. Parking Brake .......................................................................................... SET
2. Environmental Control Systems
..............................................................OFF
3. AUX BUS Switch
.....................................................................................OFF
4. Power Lever............................................................................................ IDLE
5. Propeller Control Lever
...................................................................FEATHER
(See “Section 9” of this manual for shutdown procedures for Pitch-Latched
Propellers, if equipped.)
6. Generator.................................................................................................OFF
7. Alternator
.................................................................................................OFF
8. ITT
............ STABILIZED at minimum obtainable temperature for one minute
9. Fuel Condition Lever.........................................................................CUTOFF
10. Oxygen Supply Control Switch (if on)
...................................................... OFF
11. Light Switches
.......................................................................................... OFF
12. Fuel Selector...............................................OFF if parked on a sloped surface
(Turn off the fuel valve of the higher wing to prevent fuel transfer.)
13. Avionics Master Switch
............................................................................ OFF
14. Master Switch
..........................................................................................OFF
15. Controls
............................................................................................... LOCK
16. Tie-Downs and Wheel Chocks
.............................................. AS REQUIRED
17. External Covers
................................................................................INSTALL
18. Firewall Fuel Filter
........... CHECK FILTER BYPASS FLAG (Normal – Flush)
19. Oil Dipstick/Filler Cap
....................................................CHECK HOT LEVEL
20. Oil Dipstick/Filler Cap
.............................................. CLOSED and SECURE
NOTE: If the airplane is parked on a sloped surface, it may be desirable
to turn the fuel selector valve of the higher fuel tank to the OFF position in
order to help prevent fuel transfer between tanks due to gravity.
CAUTION: Accidental moving of the fuel condition lever aft of the LOW
IDLE position, causing the
Ng
to fall below 52%, and then moving the fuel
condition lever back to LOW IDLE, can result in an ITT over-temperature
condition. If the engine begins to shutdown in this situation, allow the
engine to complete its shutdown process. Then, perform a normal engine
start using the “Engine Start” checklist.
Uncontrolled if printed