Optional Equipment
Supplemental Fuel System
CSP
−
902RFM207E
−
1
ROTORCRAFT FLIGHT MANUAL
MD900 (902 Configuration with PW 207E)
FAA Approved
Reissue 2
Original
10
−
28
PART VI
WEIGHT AND BALANCE DATA
Weight and balance characteristics:
The lateral CG of the auxiliary fuel tank is at station -2.0.
Calculate CG as shown in the example below.
EXAMPLE I: Longitudinal CG Determination
ITEM
WEIGHT
(LB)
STATION
(ARM)
MOMENT
(IN
−
LB)
Basic Weight
3512.4
738045
Pilot
185.0
130.70
24180
Copilot/Passenger
185.0
130.70
24180
Passenger - Rear Facing R/H
175.0
173.0
30275
Passenger - Rear Facing L/H
175.0
173.0
30275
Passenger - FWD Facing R/H
175.0
213.0
30275
Passenger - FWD Facing L/H
175.0
213.0
30275
1. Zero Fuel Weight
4582.4
201.1
30275
2. Add: Fuel - Main Tank Only (Jet-A)
Gross Weight:
1025.0
5607.4
191.2
199.3
195980
1117484
3. Add: Fuel - Auxiliary Tank Only
Gross Weight:
200.0
4782.4
244.8
202.9
48960
970464
4. Add: Fuel - Both Tanks
Gross Weight:
1225.0
5807.4
200.9
1166444
Summary of Contents for MD900 Explorer
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