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
5–10
CONTINUOUS OEI POWER, VY, 3500 LB
18000
17000
16000
15000
14000
12000
11000
10000
9000
8000
7000
6000
5000
4000
3000
2000
1000
0
13000
PRESSURE
AL
TITUDE − FEET
−400 −200 0 200 400 600 800 1000 1200 1400 1600
19000
20000
1800
RATE OF CLIMB AT V
Y
− FT/MIN
OAT
−10 ° C
0 ° C
10 ° C
20 ° C
40 ° C
30 ° C
50 ° C
MAXIMUM
OAT LIMIT
F92–042–12A
−1000
Figure 5–5. Single Engine Rate of Climb and Descent, From –10
°
C to 50
°
C
at V
Y
, OEI MCP, and 3500 LB Gross Weight