Category A Operations
Limitations
CSP
−
902RFM207E
−
1
ROTORCRAFT FLIGHT MANUAL
MD900 (902 Configuration with PW 207E)
FAA Approved
Reissue 2
Original
11
−
7
f927
−
034
−
1D
-20
-15
-10
-5
0
5
10
15
20
25
30
35
40
45
50
55
LIMIT
5000
5100
5200
5300
5400
5500
5600
5700
5800
5900
6000
6100
6200
6300
6400
6500
OAT -
°
C
GROSS WEIGHT - LBS (kg)
DASHED LINES FOR
AIRCRAFT WITHOUT
GENERATOR COOLING
MODIFICATION
10000 HD
LIMIT
NOTE: CABIN HEAT AND AC OFF
11000
(3353M)
10000
(3048M)
8000
(2438M)
7000
(2134M)
6000
(1829M)
5000
(1524M)
4000
(1219M)
3000
(914M)
2000
(610M)
1000
(305M)
SL
−
1000
(
−
305M)
PRESSURE
ALTITUDE - FEET
9000
(2743M)
MAXIMUM OAT
(3048M
)
(2268kg)
(2313kg)
(2359kg)
(2404kg)
(2449kg)
(2495kg)
(2540kg)
(2585kg)
(2631kg)
(2676kg)
(2722kg)
(2767kg)
(2812kg)
(2858kg)
(2903kg)
(2948kg)
(METERS)
Figure 11
−
2.2. Weight Altitude Temperature Limits
−
Clear Airfield
Summary of Contents for MD900 Explorer
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