Schweizer S300C 269C - Page 136

Weight and Balance
Pilot's Flight Manual
6-6
Reissued: 16 Jan 2019
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
SUR PLUS WEIGHT
MISSING EQUIP MENT WEIGHT
4.0 93.3 373 13 52
TO TAL BA SIC WEIGHT (DE LIVERED)
1127 100.9 113663 .4 481
MOST FOR WARD LOADING WEIGHT
(LB)
LONG.
ARM
(IN.)
LONG.
MO MENT
(IN.-LB)
LAT.
ARM
(IN.)
LAT.
MO MENT
(IN.-LB)
BA SIC WEIGHT
1127 100.9 113663 .4 481
PI LOT
170 83.2 14144 -13.8 -2346
USE ABLE FUEL
0 107.0 0
PAS SEN GER, CENTER
170 80.0 13600 .75 128
PAS SEN GER, RH
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)
BA SIC WEIGHT
1127 100.9 113663 .4 481
PI LOT
170 83.2 14144 -13.8 -2346
FUEL, FULL 30 GAL
180 107.0 19260 18 3240
FUEL, AUX 19 GAL
114 107.0 12198 -17.2 -1961
TO TAL GROSS WEIGHT
1591 100.1 159265 -.4 -586
AP PROVED AFT LIMIT 101 INCHES
Fig ure 6-4. Sam ple Weight and Bal ance Worksheet (Sheet 2 of 3)
CG OF FUEL AT STA 107.0 - S/N 004 THRU 1742 AND 1745
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 136 8/4/19 12:46 PM