Schweizer S300C 269C - Page 137

Weight and Balance
Pilot's Flight Manual
6-6.1
BA SIC WEIGHT WEIGHT
(LB)
LONG.
ARM
(IN.)
LONG.
MO MENT
(IN.-LB)
LAT.
ARM
(IN.)
LAT.
MO MENT
(IN.-LB)
WEIGHT (AS WEIGHED)
1123 100.9 113290 .4 429
THGIEW SULP RUS
MISSING EQUIP MENT WEIGHT
4.0 93.3 373 13 52
)DEREVIL ED( THGIEW CIS AB LAT OT
1127 100.9 113663 .4 481
LAT ERAL CENTER OF GRAV ITY + 0.4
GNIDAOL DRAW ROF TSOM WEIGHT
(LB)
LONG.
ARM
(IN.)
LONG.
MO MENT
(IN.-LB)
LAT.
ARM
(IN.)
LAT.
MO MENT
(IN.-LB)
THGIEW CIS AB
1127 100.9 113663 .4 481
TOL IP
170 83.2 14144 -13.8 -2346
LEUF ELBA ESU
0 108.5 0
RETNEC ,REG NES SAP
170 80.0 13600 .75 128
HR ,REG NES SAP
170 83.2 14144 13.8 2346
TO TAL GROSS WEIGHT
1637 95.0 155551 .4 609
AP PROVED FOR WARD LIMIT 95 INCHES
MOST AFT LOADING WEIGHT
(LB)
LONG.
ARM
(IN.)
LONG.
MO MENT
(IN.-LB)
LAT.
ARM
(IN.)
LAT.
MO MENT
(IN.-LB)
THGIEW CIS AB
1127 100.9 113663 .4 481
TOL IP
170 83.2 14144 -13.8 -2346
).LAG ELBA ESU 5.23( LLUF ,LEUF
195 108.5 21158 17.4 3393
TO TAL GROSS WEIGHT
1492 99.8 148965 1.0 1528
SEHCNI 101 TIMIL TFA DEVORP PA
Sam ple based on sin gle 33 gal lon fuel tank
F eru gi 6-4. Sam elp Weight and Bal ance Worksheet (Sheet 3 of 3)
Reissued:
CG OF FUEL AT STA 108.5 - S/N 1743, 1744, 1746 AND TNEUQ ES BUS
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 137 8/4/19 12:46 PM