MD Helicopters MD900 with PW206E, Flight Manual

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CSP–900RFM206E–1
Performance Data
ROTORCRAFT FLIGHT MANUAL
MD900 With PW 206E
FAA Approved
Original
5–35
F92−146−5
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
19000
20000
−10 ° C
0 ° C
10 ° C
20 ° C
40 ° C
30 ° C
50 ° C
−20 ° C
OAT
200 400 600 800 1000 1200 1400 1600 1800 2000 2200 2400 2600 0
MAXIMUM
OAT LIMIT
−30 ° C/−36 ° C
TOP, V
Y
, 6000 lb
Figure 5–29. Rate of Climb – AEO, at V
Y
, TOP, 6000 Pounds Gross Weight