MD Helicopters MD900 with PW206E, Flight Manual

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CSP–900RFM206E–1
Emergency and
Malfunction Procedures
ROTORCRAFT FLIGHT MANUAL
MD900 With PW 206E
FAA Approved
Original
3–15
3–7. ENGINE/AIRCRAFT SHUTDOWN – MANUAL
NOTE
: This procedure may be performed in the event a normal shutdown cannot be
accomplished on one or both engines.
F
Collective stick FULL DOWN
F
Cyclic stick TRIM TO NEUTRAL
F Pedals
NEUTRAL
F 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).
F
Utility panel:
F F All unnecessary bleed air and electrical
equipment
OFF
F
Fuel system panel:
F F L/R BOOST
OFF
F
Electrical master panel:
F F L/R GEN OFF
F
N
P
(s) slows to idle
CHECK
F
EEC MAN indication(s) on primary IIDS
display CHECK
F
Engine control panel:
F F L ENGINE or R ENGINE OFF
F
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).
F
IIDS CHECK NORMAL SHUTDOWN
INDICATIONS
F
Continue with normal shutdown proce
dures