Category A Operations
Performance Data
CSP
−
902RFM207E
−
1
ROTORCRAFT FLIGHT MANUAL
MD900 (902 Configuration with PW 207E)
FAA Approved
Reissue 2
Revision 4
11
−
36
f927
−
036
300
500
700
900
1100
1300
1500
1700
1900
0
10
20
30
40
50
−
10
−
20
SL
TAKEOFF DISTANCE
FEET (METERS)
OAT
−
°
C
GROSS WEIGHT - POUNDS
PRESSURE
ALTITUDE - FEET
(METERS)
(KILOGRAMS)
6500
5500
6000
5000
(2268kg)
(2495kg)
(2722kg)
(2948kg)
-1000
(-305M)
10000 HD
LIMIT
(3048M
)
1000
(305M)
2000
(610M)
3000
(914M)
4000
(1219M)
5000
(1524M)
6000
(1829M)
7000
(2134M)
10000
(3048M)
8000
(2438M)
9000
(2743M)
(91M)
(152M)
(213M)
(274M)
(335M)
(396M)
(457M)
(518M)
(579M)
Figure 11
−
5.1. Distance Required to Clear a 35 FT (11M) Obstacle on Takeoff
(Clear Airfield)
Summary of Contents for MD900 Explorer
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