Optional Equipment
Removable Copilot Controls
CSP
−
902RFM207E
−
1
ROTORCRAFT FLIGHT MANUAL
MD900 (902 Configuration with PW 207E)
FAA Approved
Reissue 2
Original
10
−
53
PART VI
WEIGHT AND BALANCE DATA
Use the weight information listed below to determine C.G. shift following control
removal or installation.
ITEM
WEIGHT
(LB)
LONGITUDINAL
STATION
(ARM)
LATERAL
STATION
(ARM)
MOMENT
(IN
−
LB)
Longitudinal Lateral
Collective control
3.60
142.35
-27.60
512.46
-99.36
Cyclic
3.11
119.86
-15.70
372.77
-48.82
Cyclic boot
0.28
118.65
-15.85
33.22
-42.29
Pedal cover
0.56
101.14
-15.85
56.64
−
8.88
Cyclic hole cover
0.45
120.00
-15.85
54.00
-7.13
Summary of Contents for MD900 Explorer
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