MD Helicopters MD900 with PW206E, Flight Manual

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CSP–900RFM206E–1
ROTORCRAFT FLIGHT MANUAL
MD900 With PW 206E
Weight and
Balance Data
Original
6–6
Weighed by
Model Serial No. Reg. No.
J. Doe
MD900 900−000XX N92XXX 12/23/XX
Date
AIRCRAFT ACTUAL WEIGHT
FUEL
OIL, ENGINE LH
OIL, ENGINE RH
OIL, TRANSMISSION
HYDRAULIC FLUID
X
EMPTY FULL
X
X
X
X
220
200
180
160
140
120
100
80
60
220
200
180
160
140
120
100
80
60
60 80 100 120 140 180 200 220 240 260 280 300 320 340 360 380 400 420 440 460 160
5
°
0"
F92–187
WL 106
FLOOR
AFT JACK
POINT
STA 233.0
BL 23.3
FWD JACK
POINT
STA 154.1
BL 0.0
NOTE: IN A LEVEL ATTITUDE, MAIN ROTOR MAST IS TILTED 3 DEG. FORWARD.
WEIGHING POINT
AVE. SCALE
READING
LBS
TARE OR
CALIB. CORR.
LBS
NET
WEIGHT
LBS
LONGITUDINAL
ARM
IN
LATERAL
ARM
IN
LONGITUDINAL
MOMENT
IN−LBS
LATERAL
MOMENT
IN−LBS
Forward 869.7 0.0 869.7 154.0 −9.3 133929 −8066
Aft Right 1289.5 0.0 1289.5 233.0 23.3 300454 29981
Aft Left 887.5 0.0 887.5 233.0 −23.3 206788 −20634
TOTAL (AS WEIGHED) 3046.7 210.4 0.4 641170 1280
Less : Surplus Weight (See Table 1) −1.8 189.4 −10.4 −346 19
Plus: Missing Required Equipment (See Table 1) 222.6 198.0 0.0 44071 0
TOTAL − BASIC WEIGHT 3267.4 209.6 0.4 684895 1299
Figure 6–5. Sample Weight and Balance Report