CSP–900RFM206E–1
Normal Procedures
ROTORCRAFT FLIGHT MANUAL
MD900 With PW 206E
FAA Approved
Original
4–9
F
Pitch change links
CHECK
F
Striker plates and rollers
CHECK
F
Inner flexbeam attach points
CHECK
F
Flexbeam lead and lag legs
CHECK
F
Upper and lower damper and damper caps
CHECK
F
Elastomeric feathering bearing
CHECK
F
Pitch change housing
CHECK
F
Blade attach pins
CHECK
F
Blade attach points
CHECK
F
Rotor blades
CHECK
F
Top of rotor head
CHECK
FUSELAGE – RIGHT REAR
F
Fuselage skin
CHECK
F
Exhaust ejector cowl
CHECK
F
Baggage door:
F
F
Handle
OPERATION
F
F
Skin
CHECK
F
F
Door strut
CHECK
F
F
Rear spoiler
CHECK
F
F
Hinge pins
CHECK
F
F
Environmental control system vent
CHECK
F
Baggage compartment:
F
F
Loose items
SECURED
F
F
Circuit breaker panel
CHECK
F
F
Baggage door
CLOSED AND LATCHED
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