MD Helicopters MD900 with PW206E, Flight Manual

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CSP–900RFM206E–1
ROTORCRAFT FLIGHT MANUAL
MD900 With PW 206E
Performance Data
FAA Approved
Original
5–12
18000
17000
16000
15000
14000
12000
11000
10000
9000
8000
7000
6000
5000
4000
3000
2000
1000
0
13000
PRESSURE
AL
TITUDE − FEET
−600 −400 −200 0 200 400 600 800 1000 1200 1400 1600
19000
20000
OAT
−10 ° C
0
° C
RATE OF CLIMB AT V
Y
− FT/MIN
F92–042–1A
Continuous OEI Power, Vy, 4000 lb
10 ° C
20 ° C
40 ° C
30 ° C
50 ° C
MAXIMUM
OAT LIMIT
−1000
Figure 5–7. Single Engine Rate of Climb and Descent, From –10
°
C to 50
°
C
at V
Y
, OEI MCP, and 4000 LB Gross Weight