CSP
−
902RFM207E
−
1
ROTORCRAFT FLIGHT MANUAL
MD900 (902 Configuration with PW 207E)
Performance Data
5
−
42
FAA Approved
Reissue 2
Revision 5
0
1000
2000
3000
4000
5000
6000
7000
8000
9000
10000
11000
12000
13000
14000
15000
16000
300
500
700
900
1100
1300
1500
1700
1900
2100
Pressure Altitude
−
ft
OAT
−
o
C
f927
−
021
−
7a
Rate of Climb and Descent
−
ft/min
TOP, V
Y
, 6500 LB
50
30
40
20
10
0
-10
-20
-36
-30
52
°
OAT LIMIT
40.6
°
OAT LIMIT
14000 FT HD
LIMIT
Figure 5
−
35. Rate of Climb
−
AEO at V
Y
TOP
−
6500 lb Gross Weight
Summary of Contents for MD900 Explorer
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