CSP
−
902RFM207E
−
1
Performance Data
ROTORCRAFT FLIGHT MANUAL
MD900 (902 Configuration with PW 207E)
FAA Approved
Reissue 2
Revision 5
5
−
53
f927
−
015
−
9
4600
4700
4800
4900
5000
5100
5200
5300
5400
5500
5600
5700
5800
5900
6000
6100
6200
6300
6400
6500
6600
6700
6800
6900
−
50
−
40
−
30
−
20
−
10
0
10
20
30
40
50
60
11000
10000
9000
7000
6000
13000
14000
15000
16000
8000
5000
4000
3000
PRESSURE ALTITUDE - FEET
THIS CHART BASED ON WINDS 3KTS OR LESS AND 15% ELECTRICAL LOAD. FOR ELECTRICAL LOADS ABOVE/BELOW
15%, DECREASE/INCREASE WEIGHT CAPABILITY 35 LBS PER 10% CHANGE IN ELECTRICAL LOAD.
REDUCE WEIGHT CAPABILITY 40 LBS WITH A/C ON
15300 H
D
12000
OAT
°
C
MAXIMUM
TEMPERATURE
FOR CABIN HEAT ON
GROSS WEIGHT
−
LB
AIRCRAFT WITHOUT
GENERATOR COOLING
MODIFICATION
NOTE: MAXIMUM INTERNAL GROSS WEIGHT 6770 LB. WEIGHTS IN EXCESS OF 6770 LB MUST BE EXTERNAL AND JETTISONABLE
Figure 5
−
45. Hover Ceiling, OGE, IPS Installed, Takeoff Power
,
Cabin Heat On
Summary of Contents for MD900 Explorer
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