CSP
−
902RFM207E
−
1
ROTORCRAFT FLIGHT MANUAL
MD900 (902 Configuration with PW 207E)
Handling Servicing
and Maintenance
Revision 4
8
−
48
Reissue 2
MANUAL ENGINE SHUTDOWN CHECK
NOTE
:
This procedure should be performed with engine control switch in IDLE and all
unnecessary bleed air and electrical equipment, including generator, OFF.
Twist grip
IDLE DETENT
N
P
slows to idle
CHECK
EEC MAN indication on primary IIDS dis
play
CHECK
Twistgrip
SNAP TO CUTOFF
Engine control switch
OFF
IIDS
CHECK NORMAL SHUTDOWN
INDICATIONS
N
G
zero percent
CHECK
EEC RESET button
PRESS
Twistgrip
PLACE IN NORMAL DETENT
DO NOT return twist grip to the NORMAL detent until N
G
is at zero
and the EEC RESET button is pressed. Failure to follow this
procedure may cause a re
−
light with a subsequent EGT
exceedance.
EEC MAN indication
CHECK OFF
CAUTION
Summary of Contents for MD900 Explorer
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