CSP
−
902RFM207E
−
1
ROTORCRAFT FLIGHT MANUAL
MD900 (902 Configuration with PW 207E)
Performance Data
5
−
8
FAA Approved
Reissue 2
Revision 5
f927
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011
20
25
30
35
40
45
50
55
60
65
70
75
80
INDICATED AIRSPEED - KNOTS
0
2000
4000
6000
8000
10000
12000
14000
16000
18000
20000
DENSITY
AL
TITUDE - FEET
Figure 5
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3. Best Rate of Climb Speed (V
Y
)
Summary of Contents for MD900 Explorer
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