S2R-H80 Single & Dual Cockpit
AIRPLANE FLIGHT MANUAL
AFM H8001 SINGLE & DUAL COCKPIT Revision B Page 27
FAA APPROVED: 3/19/2015
After clearing the runway:
a. Flaps RETRACT
Engine Shutdown:
a. Parking Brakes SET
b. Power Lever IDLE
c. Propeller Lever FEATHERED
d. Avionics OFF
e. Fuel Condition Lever CUT OFF
f. Generator Switch OFF
g. Main fuel pump switch OFF
h. Battery Switch OFF
NOTE:
During the shutdown, be sure that the gas generator
decelerates freely. Minimum run down time is 18 seconds.
NOTE:
Allow the engine to stabilize at idle for a minimum of 5 (five)
minutes before shutting down for maximum engine longevity.
IF THERE IS ANY EVIDENCE OF COMBUSTION
WITHIN THE ENGINE AFTER SHUTDOWN, PROCEED
IMMEDIATELY AS DESCRIBED UNDER “DRY
MOTORING RUN” UNTIL THERE IS NO LONGER ANY
EVIDENCE OF COMBUSTION.
NOTE:
Engine must be cooled down for 5 (five) minutes at ground idle
before engine shutdown.
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