MD Helicopters MD900 with PW206E, Flight Manual

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CSP–900 RFM206E–1
Increased Internal
Gross Weight Operations
ROTORCRAFT FLIGHT MANUAL
Model MD 900 With PW 206E
FAA Approved
Original
11–5
10 ° C
30 ° C
40 ° C
50 ° C
MAXIMUM
OAT LIMIT
OAT
RATE OF CLIMB/DESCENT AT V
Y
− FT/MIN
10000
9000
8000
7000
6000
5000
4000
3000
2000
1000
0
PRESSURE
AL
TITUDE − FEET
−400 −300 −200 −100 0 100 200 300 400 500
−10 ° C
−20 ° C
−30 ° C
−36 ° C
20 ° C
0 ° C
F90–166
5000 FT H
D
Figure 11–6. Single Engine Rate of Climb and Descent, at V
Y
, OEI MCP,
6500 LBS Gross Weight