CSP–900RFM206E–1
Normal Procedures
ROTORCRAFT FLIGHT MANUAL
MD900 With PW 206E
FAA Approved
Original
4–7
F
Oil cooler
CHECK LEAKS
F
Forward access door
CHECK OPERATION AND CONDITION;
CLOSE
RIGHT CENTER TRANSMISSION DECK
F
Oil cooler:
F
F
Cooling air inlet
NO OBSTRUCTIONS
F
F
Oil cooler
CHECK MOUNTING AND CONDITION
F
F
Air ducts
CHECK MOUNTING AND CONDITION
F
Transmission:
F
F
Transmission oil level
CHECK
F
F
Transmission oil filler cap
CHECK SECURITY
F
Static mast support
CHECK MOUNTING AND CONDITION
F
Forward outside engine mount
CHECK MOUNTING AND CONDITION
F
Engine drive shaft
CHECK
F
Fan drive shaft
CHECK
F
Rotor brake
CHECK
F
Transmission deck
CHECK FOR FOREIGN OBJECTS AND
SIGNS OF FLUID LEAKAGE
F
Engine accessory gear box
CHECK FITTINGS, LINES, CONNECTORS
AND WIRING
F
Engine oil level
CHECK: IF SIGHT GLASS IS DARK, OIL
LEVEL IS FULL
F
Engine oil filter
CHECK BYPASS INDICATOR
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. If oil level is in doubt, check at filler
dipstick (Ref Section VIII)
Summary of Contents for MD900 with PW206E
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