CSP–900RFM206E–1
Normal Procedures
ROTORCRAFT FLIGHT MANUAL
MD900 With PW 206E
FAA Approved
Original
4–13
F
Environmental control system:
(if installed)
F
F
Evaporator
CHECK
F
F
Freon lines
CHECK
F
F
Air ductwork
CHECK CONDITION
F
Transmission deck
CHECK FOR FOREIGN OBJECTS AND
SIGNS OF FLUID LEAKAGE
F
Transmission oil filter
CHECK BYPASS INDICATOR (REF.
SECTION VIII)
F
Oil cooler
CHECK LEAKS
F
Forward access door
CHECK OPERATION AND CONDITION;
CLOSE
LEFT 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
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
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