CSP–900RFM206E–1
Normal Procedures
ROTORCRAFT FLIGHT MANUAL
MD900 With PW 206E
FAA Approved
Original
4–11
LEFT REAR FUSELAGE
F
Fuselage skin
CHECK
F
Exhaust ejector cowl
CHECK
F
Work platforms/steps
CHECK
FUSELAGE – LEFT SIDE
F
Landing gear:
CHECK
F
F
Aft crosstube and damper fluid level
CHECK (REF. SECTION VII)
F
F
Passenger step
CHECK
F
F
Skid tube and abrasion strips
CHECK
F
F
Forward spacer fitting; crosstube
CHECK
F
F
Skid tube step
SECURITY, CONDITION
F
Underside of fuselage:
F
F
Fuel catch can drain (if installed)
DRAIN
F
F
Fuselage skin
CHECK
F
Left side passenger door:
F
F
Upper and lower track and guide
CHECK
F
F
Door rollers
CHECK OPERATION
F
F
Door skin and glass
CHECK
F
F
Door stops/pins
CHECK
F
Left side passenger compartment:
F
F
Upholstery
CHECK CONDITION
F
F
Seats and seat belts
CHECK OPERATION
F
F
Loose equipment
STOWED
NOTE:
Nothing stowed under seats that are to be occupied.
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