CSP
−
902RFM207E
−
1
Performance Data
ROTORCRAFT FLIGHT MANUAL
MD900 (902 Configuration with PW 207E)
FAA Approved
Reissue 2
Revision 5
5
−
63
500
550
600
650
700
750
800
850
900
−
40
−
20
0
20
40
60
PRESSURE ALTITUDE - FEET
4000
8000
SEA LEVEL
16000
12000
AMBIENT TEMPERATURE (
°
C)
f927
−
019
Figure 5
−
51. EGT Chart
Summary of Contents for MD900 Explorer
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