CSP
−
902RFM207E
−
1
ROTORCRAFT FLIGHT MANUAL
MD900 (902 Configuration with PW 207E)
Additional Operations
and Performance Data
Original
9
−
7
Reissue 2
f927
−
026
−
3a
6,000 lb.
5,000 lb.
4,000 lb.
MCP limit
6250 lb.
Long range cruise
6500 lb.
200
250
300
350
400
450
500
550
INDICATED AIR SPEED - KNOTS
FUEL
FLOW - LB/HR
40
50
60
70
80
90
100
110
120
130
140
150
Figure 9
−
3. Fuel Flow, AEO, 8000 Feet H
P
, ISA (
−
1
°
C)
Summary of Contents for MD900 Explorer
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