CSP
−
902RFM207E
−
1
ROTORCRAFT FLIGHT MANUAL
MD900 (902 Configuration with PW 207E)
Performance Data
5
−
20
FAA Approved
Reissue 2
Revision 5
f927
−
012
−
13b
-1000
0
1000
2000
3000
4000
5000
6000
7000
8000
9000
10000
11000
12000
13000
14000
15000
16000
17000
18000
19000
20000
-600
-400
-200
0
200
400
600
800
1000
1200
1400
1600
PRESSURE
AL
TITUDE - FEET
OAT -
5
C
RATE OF CLIMB AT V
Y
- FT/MIN
−
30
−
20
−
36
30
40
50
20
10
0
-10
52
°
OAT LIMIT
40.6
°
OAT LIMIT
Figure 5
−
14. Single Engine Rate of Climb and Descent, at V
Y
, OEI MCP,
and 5750 LB Gross Weight
Summary of Contents for MD900 Explorer
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