CSP
−
902RFM207E
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1
ROTORCRAFT FLIGHT MANUAL
MD900 (902 Configuration with PW 207E)
Emergency and
Malfunction Procedures
FAA Approved
Reissue 2
Original
3
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14
3
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7.
ENGINE/AIRCRAFT SHUTDOWN
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MANUAL
NOTE
:
This procedure may be performed in the event a normal shutdown cannot be
accomplished on one or both engines.
Collective stick
FULL DOWN
Cyclic stick
TRIM TO NEUTRAL
Pedals
NEUTRAL
Twist grip(s)
IDLE DETENT
NOTE
:
The idle position is not marked on the twist grips. Idle is located at the point where
the twist grip can no longer be rotated toward the OFF position without applying
additional force (approximately 30 to 40 LBS).
Utility panel:
All unnecessary bleed air and electrical
equipment
OFF
Fuel system panel:
L/R BOOST
OFF
Electrical master panel:
L/R GEN
OFF
N
P
(s) slows to idle
CHECK
EEC MAN indication(s) on primary IIDS
display
CHECK
Engine control panel:
L ENGINE or R ENGINE
OFF
Twistgrip(s)
SNAP TO CUTOFF
NOTE
:
AT a point between NORMAL and OFF, the twist grip will no longer able to be
rotated toward the OFF position without applying additional force (approximately
30 to 40 LBS).
IIDS
CHECK NORMAL SHUTDOWN
INDICATIONS
Continue with normal shutdown proce
dures
Summary of Contents for MD900 Explorer
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