CSP
−
E
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1
Weight and Balance Data
ROTORCRAFT FLIGHT MANUAL
MD 500E
(Model 369E)
Revision 14
6
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7
W
EIGHT
AND
B
ALANCE
R
EPORT
M
ODEL
500
WEIGHED BY: J. Doe DATE 4 October 1982
MODEL 369E SERIAL NO.
REGISTRATION NO.
WEIGHING
POINTS
SCALE
READING
(LBS)
TARE OR
CALIBRATION
CORRECTION
(LBS)
NET
WEIGHT
(LBS)
ARM
(IN.)
MOMENT
(IN. LB)
LEFT MAIN
721.7
0.0
721.7
96.9
69933
RIGHT MAIN
591.7
0.0
591.7
96.9
57915
TAIL
182.0
0.0
182.0
197.2
35890
TOTAL UNADJUSTED NET WEIGHT
1495.4
109.1
163138
TOTAL WEIGHT OF SURPLUS EQUIPMENT (SEE TABLE 1)
−
1.3
96.9
−
126
TOTAL WEIGHT OF MISSING EQUIPMENT (SEE TABLE 1)
15.9
97.4
+1549
TOTAL BASIC WEIGHT
1510.0
109.0
164561
REFER TO THE OWNER’S MANUAL FOR C.G. LIMITS APPLICABLE FOR GROSS WEIGHT RANGE
FUEL/OIL AT TIME OF WEIGHING
EMPTY
FULL
FUEL
X
ENGINE OIL
X
MAIN GEAR BOX
X
TAIL GEAR BOX
X
Figure 6
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4. Sample Weight and Balance Report (Sheet 1 of 2)
