CSP
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902RFM207E
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1
Limitations
ROTORCRAFT FLIGHT MANUAL
MD900 (902 Configuration with PW 207E)
FAA Approved
Reissue 2
Revision 4
2
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7
2
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5.
CENTER OF GRAVITY (CG ENVELOPE)
Make sure the rotorcraft CG and weight are within approved limits throughout
flight operations.
Expanded lateral CG:
Maximum lateral CG for takeoffs and landings from/to a surface is +2 inches.
V
NE
is 60 KIAS with lateral CG more than +2 inches.
Longitudinal CG envelope is as shown on chart “B” below when lateral CG is
greater than +2 inches.
EXPANDED
CG LIMITS
DURING OPERATION IN THE
EXPANDED CG REGION OF
CHART A, THE MAXIMUM LON
GITUDINAL CG LIMIT, AS DE
PICTED BY THE DASHED LINE
IN CHART B, APPLIES.
5100 LB
CHART A
: LATERAL CG STATION (INCH)
GROSS WEIGHT - LB
GROSS WEIGHT - LB
CHART B
: LONGITUDINAL CG STATION (INCH)
7000
6770
6000
5500
5000
4500
4000
3500
3000
6500
7000
6770
6000
5500
5000
4500
4000
3500
3000
6500
194
196
198
200
202
204
206
208
-3
-2
-1
0
1
2
3
4
5
6
7
FM02
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006
Figure 2
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6. Center of Gravity Envelope
Summary of Contents for MD900 Explorer
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