CSP
−
902RFM207E
−
1
ROTORCRAFT FLIGHT MANUAL
MD900 (902 Configuration with PW 207E)
Performance Data
5
−
62
FAA Approved
Reissue 2
Revision 5
f927
−
018
-20
-10
0
10
20
30
40
35
40
45
50
55
60
65
70
75
80
ENGINE T
ORQUE (%)
AMBIENT TEMPERATURE (
°
C)
50
12000
6000
8000
14000
16000
10000
4000
2000
-30
-36
SEA LEVEL
PRESSURE ALTITUDE (FEET)
Figure 5
−
50. Engine Torque Chart
Summary of Contents for MD900 Explorer
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