MD Helicopters MD900 with PW206E, Flight Manual

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CSP–900 RFM206E–1
ROTORCRAFT FLIGHT MANUAL
Model MD 900 With PW 206E
Increased Internal
Gross Weight Operations
FAA Approved
Original
11–6
F90–167–1
10000
9000
8000
7000
6000
5000
4000
3000
2000
1000
0
PRESSURE AL
TITUDE
–
FEET
RATE OF CLIMB AT V
Y
− FT/MIN
OAT
−30 ° C −36 ° C
−20 ° C
−10 ° C
0 ° C
10 ° C
20 °
C
30 ° C
40 ° C
400 600 800 1000 1200 1400 1600 1800 2000
50 ° C
MAXIMUM
OAT LIMIT
5000 FT H
D
Figure 11–7. Twin Engine Rate of Climb, at V
Y
, MCP, 6500 Pounds Gross Weight