CSP
−
902RFM207E
−
1
ROTORCRAFT FLIGHT MANUAL
MD900 (902 Configuration with PW 207E)
Normal Procedures
FAA Approved
Reissue 2
Original
4
−
22
4
−
4.
ENGINE PRE
−
START COCKPIT CHECK
ELECTRICAL POWER
−
OFF
All cabin doors closed and safelocked
CHECK
Seat belt and shoulder harness for proper fit and engage
ment of buckle
FASTENED
Operation of shoulder harness inertia lock
CHECK
Rotor brake
STOWED
Magnetic compass
CHECK
Flight instruments
CHECK STATIC
POSITION/SET
Collective Control:
Collective friction
ON
Collective stick position
FULL DOWN
If collective is not full down, do not try to force down until hydraulic
pressure increases during start.
Twistgrip alignment marks aligned with index mark
CHECK
LDG/HVR lights
OFF
Key switch
ON
Essential bus panels:
Circuit breakers
IN
NACA inlet panel (if installed):
NACA inlet switch
NORMAL
Utility panel:
CAB HEAT
OFF
AC/VENT
OFF
PITOT HEAT (if installed)
OFF
IPS (if installed)
OFF
VSCS L/R
ON
CAUTION
Summary of Contents for MD900 Explorer
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