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
5–56
F92–050–1
NG− %
−36 −40 −30 −20 −10 0 10 20 30 40 50
AMBIENT TEMPERATURE (‘C)
82
83
84
85
86
87
88
89
90
91
92
93
94
95
96
PRESSURE ALTITUDE − FEET
8000
16000
12000
4000
SEA
LEVEL
81
Figure 5–45. N
G
Chart – (N
G
read from Secondary IIDS Display)