CSP
−
902RFM207E
−
1
Performance Data
ROTORCRAFT FLIGHT MANUAL
MD900 (902 Configuration with PW 207E)
FAA Approved
Reissue 2
Revision 5
5
−
23
F927
−
107b
0
1000
2000
3000
4000
5000
6000
7000
8000
9000
−
200
−
100
0
100
200
300
400
500
-30
°
C
-36
°
C
-20
°
C
-10
°
C
0
°
C
10
°
C
20
°
C
30
°
C
5000 FT H
D
40
°
C
40.6
°
C
OAT LIMIT
50
°
C
52
°
C
OAT LIMIT
THIS CHART BASED ON ELECTRICAL LOAD OF 30%,
HEATER OFF, AND AIR-CONDITIONING OFF
PRESSURE AL
TITUDE
−
FEET
OAT
RATE OF CLIMB AT V
Y
- FT/MIN
Continuous OEI Power, Vy, 6500 lb
Figure 5
−
17. Single Engine Rate of Climb and Descent, at V
Y
, OEI MCP,
6500 LBS Gross Weight
Summary of Contents for MD900 Explorer
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