CSP
−
902RFM207E
−
1
ROTORCRAFT FLIGHT MANUAL
MD900 (902 Configuration with PW 207E)
Normal Procedures
FAA Approved
Reissue 2
Original
4
−
8
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 and latched
CHECK
FUSELAGE
−
RIGHT TOP REAR
Work platforms/steps.
CHECK
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
Right Engine:
Engine oil access door
CHECK CONDITION
Engine oil level
CHECK
NOTE
:
To reduce the possibility of over servicing and ensure accurate readings for oil
consumption measurement, it is recommended that oil level always be checked
within 10 minutes after engine shutdown (Ref Section VIII).
Oil filler cap
CHECK
Engine cowling assembly
CHECK
Fuselage skin
CHECK CONDITION
Notar fan inlet:
Summary of Contents for MD900 Explorer
Page 4: ......
