CSP
−
902RFM207E
−
1
ROTORCRAFT FLIGHT MANUAL
MD900 (902 Configuration with PW 207E)
Normal Procedures
FAA Approved
Reissue 2
Original
4
−
14
LEFT CENTER TRANSMISSION DECK
Oil cooler:
Cooling air inlet
NO OBSTRUCTIONS
Oil cooler
CHECK MOUNTING, LEAKS AND
CONDITION
Air ducts
CHECK MOUNTING AND
CONDITION
Static mast support
CHECK MOUNTING AND
CONDITION
Forward outside engine mount
CHECK MOUNTING AND
CONDITION
Engine drive shaft
CHECK
Fan drive shaft
CHECK
Rotor brake
CHECK
Transmission deck
CHECK FOR FOREIGN OBJECTS AND
SIGNS OF FLUID LEAKAGE
Engine accessory gear box
CHECK FITTINGS, LINES,
CONNECTORS AND WIRING
Engine oil filter
CHECK BYPASS INDICATOR
Transmission access door latches, hinges,
and door
CHECK OPERATION; CLOSE
Cabin door closed/open and latched/secured
CHECK
FUSELAGE
−
LEFT TOP REAR
Engine air inlet w/o particle separator:
Inlet screen
CHECK
−
NO OBSTRUCTIONS
NACA inlet
NO OBSTRUCTIONS
Engine air inlet with particle separator:
Particle separator
CHECK
−
NO OBSTRUCTIONS
Bypass door
CLOSED, CONDITION OF SEAL
NACA inlet door
CLOSED, NO OBSTRUCTIONS
Summary of Contents for MD900 Explorer
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