WEIGHT AND BAL ANCE WORKSHEET
MODEL 269C-1 (300CB)
Weight and Balance
Pilot's Flight Manual
Reissued: 16 Jan 2019 6-5
HE LI COP TER MODEL SE RIAL NUMBER REG IS TRA TION NUMBER
269C-1 0002 N61442
DATE WEIGHED BY
6-28-95 JOHN DOE
WEIGHING POINT
SCALE NET LONG. LONG. LAT. LAT.
READING TARE WEIGHT ARM MO MENT ARM MO MENT
(LB) (LB) (LB) (IN) (IN-LB) (IN) (IN-LB)
LEFT MAIN 464 0 464 75.6 35078 -19.0 - 8816
RIGHT MAIN 496 0 496 75.6 37498 +19.0 + 9424
AFT 141 0 141 271.4 38267 +0.6 + 85
TO TAL (AS WEIGHED) 1101 0 1101 100.7 110871 +0.6 + 693
A DIS TANCE FROM STATION 100.0 TO
MAIN WEIGHING POINTS IN INCHES
RIGHT HAND
24.4
LEFT HAND
24.4
B AV ER AGE MO MENT ARM FOR
MAIN WEIGHING POINTS (100.0A)
100.0 - 24.4 = 75.6
C MO MENT ARM FOR AFT WEIGHING
POINT IN INCHES
271.4
OIL ABOARD YES NO
MAIN GEAR BOX YES NO
TAIL GEAR BOX YES NO
FULL FUEL ABOARD YES NO
EQUIP MENT MISSING AT TIME OF WEIGHING
ITEM NUMBER WEIGHT
LONG. LONG. LAT. LAT.
ARM MO MENT ARM MO MENT
300CB FLIGHT MAN UAL 1.0 48.0 48 0 0
UNUSEABLE FUEL
(SIN GLE TANK)
3.0 108.5 325 -17 -51
(UNUSEABLE FUEL
(DUAL TANK))
(12.0) (108.5) (1302) (+.2) (+2.4)
NOTE: Re mov able Por tions Of Ground Han dling Wheel In stal la tion (If So Equipped) Are NOT In cluded In Air craft Empty Weight.
TO TAL 4.0 93.3 373 -12.8 -51
SUR PLUS EQUIP MENT IN AIR CRAFT AT TIME OF WEIGHING
ITEM NUMBER
WEIGHT
LONG. LONG. LAT. LAT.
ARM MO MENT ARM MO MENT
TO TAL
Sam ple based on sin gle 33 gallon tank.
66 gal lon to tal fuel ca pac ity in stal la tion shown above in ( ).
Fig ure 6-4. Sam ple Weight and Bal ance Worksheet (Sheet 1 of 2)
X
X
X
SCHWEIZER
Model 269C-1 Helicopter
CSP book 2..indd 127 8/4/19 12:53 PM
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