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
5–3
−40 −30 −20 −10 0 10 20 30 40
−2000
0
2000
4000
6000
8000
10000
12000
14000
16000
18000
20000
DENSITY
AL
TITUDE − FEET
0.98
1.00
1.02
1.04
1.06
1.08
1.10
1.12
1.14
1.16
1.18
1.20
1.22
1.24
1.26
1.28
1.30
1.32
1.34
1.36
TEMPERATURE − ° C
TEMPERATURE − ° F
50
60
−40 −30 −20 −10 0 10 20 30 40 50 60 70 80 90 100 110
F92–039
120 130 140
Figure 5–1. Density Altitude Chart