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
5–24
F92–043–1
OAT
−20 ° C
−30 ° C
−36 ° C
−10 ° C
0 ° C
10 ° C
20 ° C
40 ° C
30 ° C
18000
17000
16000
15000
14000
12000
11000
10000
9000
8000
7000
6000
5000
4000
3000
2000
1000
0
13000
PRESSURE
AL
TITUDE − FEET
RATE OF CLIMB AT V
Y
− FT/MIN
MAXIMUM
OAT LIMIT
50 ° C
19000
20000
700 900 1100 1300 1500 1700 1900 2100 2300 2500 2700 2900 3100 3300 3500 3700
MCP, V
Y
, 4000 lb
Figure 5–18. Rate of Climb – AEO, at V
Y
, MCP, 4000 Pounds Gross Weight