Schweizer S300C 269C - Page 135

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
DATE WEIGHED BY
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 482 1.9 480 75.6 36288 -19.0 - 9120
RIGHT MAIN 500 1.9 498 75.6 37649 +19.0 + 9462
AFT 148 2.9 145 271.4 39353 +0.6 + 87
TO TAL (AS WEIGHED) 1130 6.7 1123 100.9 113290 +0.4 + 429
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
405 FLIGHT MAN UAL 1.0 48.0 48 0 0
UNUSEABLE FUEL
(33 gal. fuel tank)*
3.0 108.5 325 +17.4 +52
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 +13 +52
SUR PLUS EQUIP MENT IN AIR CRAFT AT TIME OF WEIGHING
ITEM NUMBER WEIGHT LONG. LONG. LAT. LAT.
ARM MOMENT ARM MO MENT
TO TAL
*Un us able fuel for 30 gal lon tank is .2 gal lon at
108.5 inch or 107 inch de pend ing on air craft S/N.
Sam ple based on sin gle 33 gal lon fuel tank con fig u ra tion
Fig ure 6-4. Sam ple Weight and Bal ance Worksheet (Sheet 1 of 3)
X
X
X
X
This Document contains technical data subject to EAR. See WARNING and classifications on first page.
SCHWEIZER
Model 269C Helicopter
CSP Book 1 CSP-C-1.indd 135 8/4/19 12:46 PM