MD Helicopters MD900 Explorer, Flight Manual

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CSP − 902RFM207E − 1
Performance Data
ROTORCRAFT FLIGHT MANUAL
MD900 (902 Configuration with PW 207E)
FAA Approved
Reissue 2
Revision 5
5 − 43
F927 − 021 − 8
0
1000
2000
3000
4000
5000
6000
7000
8000
9000
10000
1800 1850 1900 1950 2000 2050
Pressure Altitude
−
ft
Rate of Climb and Descent − FT/ MIN
OAT
3000 FT H
D
40.6
°
C
OAT LIMIT
MCP, V
Y
, 6770 lb
40
°
C
-30
°
C
-20
°
C
-10
°
C
0
°
C
10
°
C
20
°
C
30
°
C
-36
°
C
Figure 5 − 36. Rate of Climb − AEO at V
Y
TOP − 6770 lb Gross Weight