EXAMPLE WEIGHT AND BALANCE REPORT
MODEL 269D
WEIGHED BY: J. DOE DATE: 9-20-92
REGISTRATION NO.: N330T SERIAL NO.: 001 MODEL: 269D
Figure 6-5. Sample Weight and Balance Report (Sheet 1of 2)
WEIGHING
POINTS
SCALE
READING
(LBS)
TARE OR
CALIBRATION
CORRECTION
(LBS)
NET
WEIGHT
(LBS)
LONG.
ARM
(IN.)
LONG.
MOMENT
(IN.-LB.)
LAT.
ARM
(IN.)
LAT.
MOMENT
(IN.-LB.)
LEFT MAIN 448 8 440 117.25 51590 -18.625 -8195
RIGHT MAIN 408 5 403 117.25 47252 +18.625 +7506
NOSE 306 1 305 73.0 22265 +4.0 +1220
TOTAL UNADJUSTED NET WEIGHT 1148 105.5 121107 +.46 +531
LONGITUDINAL MOMENT ARM OF MAIN REACTION 117.25
LONGITUDINAL MOMENT ARM OF NOSE REACTION 73.0
LATERAL MOMENT ARM OF MAIN REACTION ± 18.625 IN.
LATERAL MOMENT ARM OF NOSE REACTION + 4.0 IN.
FUEL/OIL ABOARD AT TIME OF WEIGHING EMPTY FULL
FUEL
ENGINE OIL
MAIN GEAR BOX
TAIL GEAR BOX
MISSING EQUIPMENT AT TIME OF WEIGHING
ITEM
WEIGHT
(LBS)
LONG.
ARM (IN.)
LONG.
MOMENT
(IN.-LB.)
LAT. ARM
(IN.)
LAT.
MOMENT
(IN.-LB.)
ELT
3.0 84.0 +252 +25 +75
UNUSABLE FUEL
5.4 +104.2 +563 +24 +130
TOTAL
8.4 97.0 +815 +24.4 +205
SURPLUS EQUIPMENT AT TIME OF WEIGHING
ITEM
WEIGHT
(LBS)
LONG.
ARM (IN.)
LONG.
MOMENT
(IN.-LB.)
LAT. ARM
(IN.)
LAT.
MOMENT
(IN.-LB.)
VIBREX
-8 +65 -520 -7 +56
TOTAL
-8 +65 -520 -7 +56
X
X
X
X
Weight and Balance
Schweizer RSG, LLC.
Model 269D Helicopter
Pilot's Flight Manual
6-9
Reissued: 17 Jan 2019
Book 3.indd 147 8/4/19 1:25 PM
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