CSP
−
902RFM207E
−
1
ROTORCRAFT FLIGHT MANUAL
MD900 (902 Configuration with PW 207E)
Normal Procedures
FAA Approved
Reissue 2
Original
4
−
6
Forward spacer fitting; crosstube
CHECK
Skid tube and abrasion strips
CHECK
Aft crosstube and damper fluid level
CHECK (REF. SECTION VII)
Aft fuel vent fairing
CLEAR OF OBSTRUCTIONS
Antennas/externally mounted equip
ment
CHECK SECURITY/ATTACHMENT
Fuel sump drain:
Push in fuel drain control to take sample
CHECK FOR CONTAMINATION;
VERIFY PROPER OPERATION OF
DRAIN VALVES
Fuel drain door
CLOSED
Forward fuselage skin and steps
CONDITION
External power door, (front mounted bat
tery only) avionics access panel, static port,
fuel cap
SECURITY, CONDITION
Right side passenger door:
Upper and lower track and guide
CHECK
Door rollers
CHECK OPERATION
Door skin and glass
CHECK
Door stops/pins
CHECK
Right side passenger compartment:
Upholstery
CHECK CONDITION
Seats and seat belts
CHECK OPERATION
Cabin heat controls
AS DESIRED
Loose equipment
STOWED
NOTE
:
Nothing stowed under seats that are to be occupied.
RIGHT FORWARD TRANSMISSION DECK
Hydraulic System:
Hydraulic manifold
CHECK MOUNTING AND FLUID LEVEL
Summary of Contents for MD900 Explorer
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