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
5–57/(5–58 blank)
F92−050−2
–40 –30 –20 –10 0 10 20 30 40 50 60
AMBIENT TEMPERATURE (‘C)
83
84
85
86
87
88
89
90
91
92
93
94
95
96
97
NG
–
%
PRESSURE
ALTITUDE − FEET
16000
12000
8000
4000
20000
SEA LEVEL
Figure 5–46. N
G
Chart – (N
G
read from Third Level POWER CHECK menu)