CSP
−
902RFM207E
−
1
ROTORCRAFT FLIGHT MANUAL
MD900 (902 Configuration with PW 207E)
Emergency and
Malfunction Procedures
FAA Approved
Reissue 2
Original
3
−
12
Collective control:
NOTE
:
The following steps of rotating the twist grip to reset the PLA are not required if
the engine was previously shut down utilizing the manual shutdown procedures
7. Insure the twist grip is in the OFF position.
Twist grip on selected engine
ROTATE TO FULL OPEN (PAST
THE ‘‘NORMAL’’ DETENT): THIS
RESETS THE PLA
Twist grip on selected engine
ROTATE TO OFF
NOTE
:
AT a point between NORMAL and OFF, the twist grip will no longer be able to
be rotated toward the OFF position without applying additional force
(approximately 30 to 40 lb / 13 to 18 kg).
Electrical master panel:
Generator on selected engine
OFF
Fuel system panel:
L BOOST or R BOOST for appropriate
engine
ON, CHECK IIDS INDICATIONS
Engine control panel:
L ENGINE or R ENGINE
IDLE
Monitor EGT, N
G,
and starter limits during start. Abort the start
If EGT rises rapidly through 700
°
C.
CAUTION
Summary of Contents for MD900 Explorer
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