CSP
−
902RFM207E
−
1
Emergency and
Malfunction Procedures
ROTORCRAFT FLIGHT MANUAL
MD900 (902 Configuration with PW 207E)
FAA Approved
Reissue 2
Original
3
−
13
Abort start procedure:
Twistgrip on selected engine
OFF
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).
Engine control panel switch
OFF WHEN EGT IS BELOW 150
°
C
Twist grip for selected engine
ROTATE TOWARDS NORMAL
NOTE
:
As N
G
increases through 8% rotate twistgrip toward normal until lightoff occurs.
Observe EGT indication for immediate temperature rise. Monitor EGT and N
G
during start. Increase twistgrip toward normal only as necessary to keep N
G
accelerating toward idle. Manually bring N
P
/N
R
to 65%.
If lightoff is not attained with an increase of EGT and N
G
within
10 seconds, rotate the twistgrip to OFF and place the engine control
switch to off. Following a 30 second fuel drain period, perform a
30 second dry motoring run (Ref. Section VIII) before attempting
another start. Repeat the complete starting sequence observing
limitations.
Engine oil pressure
CHECK
Generator
ON
IIDS
CHECK
GPU start only:
Generators
ON
GPU
DISCONNECT
CAUTION
Summary of Contents for MD900 Explorer
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