CSP
−
902RFM207E
−
1
ROTORCRAFT FLIGHT MANUAL
MD900 (902 Configuration with PW 207E)
Normal Procedures
FAA Approved
Reissue 2
Original
4
−
7
System filters
CHECK IMPENDING BYPASS
INDICATORS (REF. SECTION VIII)
Longitudinal hydraulic actuator
CHECK LEAKS, MOUNTING
Hydraulic lines
CHECK LEAKS, FITTINGS
Static mast supports
CHECK ATTACHMENT
Rotor brake fluid level
CHECK (IF INSTALLED)
Environmental control system:
Air inlet screen
CHECK
Cabin air and fan plenum
CHECK MOUNTING
Air ductwork
CHECK CONDITION
Generator cooling ducts (if installed)
CHECK CONDITION
Transmission deck
CHECK FOR FOREIGN OBJECTS AND
SIGNS OF FLUID LEAKAGE
Forward access door
CHECK OPERATION AND CONDITION;
CLOSE
Generator cooling inlet (if installed)
CHECK
RIGHT CENTER TRANSMISSION DECK
Oil cooler:
Cooling air inlet
NO OBSTRUCTIONS
Oil cooler
CHECK MOUNTING, LEAKS AND
CONDITION
Air ducts
CHECK MOUNTING AND CONDITION
Transmission:
Transmission oil level
CHECK
Transmission oil filler cap
CHECK SECURITY
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
Summary of Contents for MD900 Explorer
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