CSP
−
902RFM207E
−
1
Performance Data
ROTORCRAFT FLIGHT MANUAL
MD900 (902 Configuration with PW 207E)
FAA Approved
Reissue 2
Revision 5
5
−
33
f927
−
081b
0
1000
2000
3000
4000
5000
6000
7000
8000
9000
10000
11000
12000
13000
14000
15000
16000
17000
18000
19000
20000
0
200
400
600
800
1000
1200
1400
1600
1800
2000
Rate of Climb
−
ft/min
Pressure Altitude
−
ft
OAT
−
o
C
52
°
OAT LIMIT
40.6
°
OAT LIMIT
14000 FT HD
LIMIT
MCP, V
Y
, 6500 lb
30
50
20
10
0
-10
-30
-36
-20
40
Figure 5
−
26. Rate of Climb
−
AEO at V
Y
MCP
−
6500 lb Gross Weight
Summary of Contents for MD900 Explorer
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