TM 1-1510-218-10
8-23
are at HIGH IDLE before initiating the final approach.
Perform the following checks.
1. Power – As required.
2. GEAR – UP.
3. FLAPS – APPROACH.
4. FLAPS (105 KIAS) – UP.
5. LANDING LIGHTS – OFF.
6. Climb power – Set.
7. YD – As required.
8. BRAKE DEICE – OFF.
8-44. AFTER LANDING.
Complete the following procedures after the
aircraft has cleared the runway.
1. CONDITION levers – As required.
2. ENG AUTO IGN – OFF.
3. ICE & RAIN switches – As required.
4. FLAPS – As required.
5. XPNDR – Standby.
6. RADAR – Standby.
7. LIGHTS – As required.
8-45. ENGINE SHUTDOWN.
NOTE
To prevent sustained loads on rudder
shock links, the aircraft should be parked
with the nose gear centered.
1. BRAKE DEICE – OFF.
2. Parking brake – Set.
3. LANDING/TAXI light – OFF.
4. CABIN TEMP MODE switch – OFF.
5. AUTOFEATHER switch – OFF.
6. VENT and AFT VENT BLOWER switches
– AUTO.
7. INVERTER switches – OFF.
8. Battery condition – Check as required. If
BATTERY CHARGE light is illuminated
during engine shutdown, turn BATT switch
OFF momentarily and note loadmeter
reading. After 90 seconds, momentarily
turn switch OFF again and note loadmeter
reading.
Battery
condition
is
unsatisfactory if BATTERY CHARGE light
remains illuminated and charge current
fails to decrease between checks.
CAUTION
Monitor TGT/ITT during shutdown. If
sustained
combustion
is
observed,
proceed
immediately
to
Abort
Start
procedure, Paragraph 8-24.
9. TGT/ITT – Check. TGT/ITT must be
660
C or below for 1 minute prior to
shutdown.
10. CONDITION levers – FUEL CUTOFF.
11. PROP levers – FEATHER.
Do not turn EXTERIOR LIGHTS off until
propeller rotation has stopped.
12. EXTERIOR LIGHTS – Off.
13. MASTER PANEL LIGHTS – Off.
14. AVIONICS MASTER switch – Off.
15. MASTER SWITCH – Off.
16. Key lock switch – OFF.
17. Oxygen system – OFF.
18. Chocks – As required.
19. Parking brake – As required.
20. Control locks – As required.
8-46. BEFORE LEAVING AIRCRAFT.
1. Wheels – Chocked.
WARNING
