CSP
−
902RFM207E
−
1
ROTORCRAFT FLIGHT MANUAL
MD900 (902 Configuration with PW 207E)
Normal Procedures
FAA Approved
Reissue 2
Original
4
−
13
Crew Seat
CONDITION
−
NOTHING STOWED
UNDER SEAT
NOTE:
Nothing stowed under seats that are to be occupied.
Co-pilot pedals (if installed)
ADJUSTED; ADJUSTMENT PINS
ENGAGED
Crew door
CLOSE
Avionics access panel
CHECK
Static port
CHECK
−
NO OBSTRUCTIONS
Fwd fuel vent fairing
CHECK
−
NO OBSTRUCTIONS
LEFT FORWARD TRANSMISSION DECK
Hydraulic System:
Hydraulic manifold
CHECK MOUNTING AND FLUID LEVEL
System filters
CHECK IMPENDING BYPASS
INDICATORS (REF. SECTION VIII)
Lateral and collective hydraulic actua
tors
CHECK LEAKS, MOUNTING
Hydraulic hand pump
CHECK LEAKS, FITTINGS
Hydraulic lines
CHECK LEAKS, FITTINGS
Static mast supports
CHECK ATTACHMENT
Environmental control system:
(if installed)
Evaporator
CHECK
Freon lines
CHECK
Air ductwork
CHECK CONDITION
Transmission deck
CHECK FOR FOREIGN OBJECTS AND
SIGNS OF FLUID LEAKAGE
Transmission oil filter
CHECK BYPASS INDICATOR (REF.
SECTION VIII)
Generator cooling ducts (if installed)
CHECK CONDITION
Forward access door
CHECK OPERATION AND CONDITION;
CLOSE
Generator cooling inlet (if installed)
CHECK
Summary of Contents for MD900 Explorer
Page 4: ......
