CSP
−
902RFM207E
−
1
ROTORCRAFT FLIGHT MANUAL
MD900 (902 Configuration with PW 207E)
Normal Procedures
FAA Approved
Reissue 2
Original
4
−
10
FUSELAGE
−
RIGHT REAR
Fuselage skin
CHECK
Exhaust ejector cowl
CHECK
Baggage door:
Handle
OPERATION
Skin
CHECK
Door strut
CHECK
Rear spoiler
CHECK
Hinge pins
CHECK
Environmental control system vent
CHECK
Baggage compartment:
Loose items
SECURED
Circuit breaker panel
CHECK
Fan Control Rod Spring Capsule:
• • •
Baggage compartment ceiling panel
UNZIP
• • •
Control rod spring capsule
CHECK
NOTE
:
Check piston rod for movement, clips installed on outer bellcrank assembly and
lanyards connected to clips. If clips are bent and/or lanyards are taut, or piston
rod moves in any direction, advise maintenance.
• • •
Baggage compartment ceiling panel
ZIP UP
Baggage door
CLOSED AND LATCHED
Antennas/externally mounted equip
ment
CHECK SECURITY/ATTACHMENT
TAILBOOM AND EMPENNAGE
−
RIGHT SIDE
Tailboom attach ring
CHECK
Tailboom slots
CLEAR OF OBSTRUCTIONS
Tailboom
CHECK CONDITION
Horizontal stabilizer:
Horizontal stabilizer attach points
CHECK
Horizontal stabilizer fairing
CHECK
Antennas
CHECK SECURITY/ATTACHMENT
Vertical stabilizer
CHECK
Nav light/strobe lenses
CHECK
Summary of Contents for MD900 Explorer
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