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) 1,101 100.7 110,871
SUR PLUS WEIGHT
MISSING EQUIP MENT WEIGHT 4.0 93.3 373
TO TAL BA SIC WEIGHT (DE LIVERED) 1,105 100.7 111,244
LAT. CENTER OF GRAV ITY + 0.6
MOST FOR WARD LOADING WEIGHT
(LBS)
LONG.
ARM
(IN.)
LONG.
MO MENT
(IN.-LB)
LAT.
ARM
(IN.)
LAT.
MO MENT
(IN.-LB)
BA SIC WEIGHT 1,105 100.7 111,274
PI LOT AND PAS SEN GER L.H. 340 83.2 28,288
USE ABLE FUEL 0.0 108.5 0
TO TAL GROSS WEIGHT 1,445 96.6 139,562
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 1,105 100.7 111,274
PI LOT 170.0 83.2 14,144
FUEL, FULL 32.5 GAL. (USE ABLE) 195 108.5 21,158
(FUEL, AUX 64 GAL. (USE ABLE)) (384) (108.5) (41,664)
TO TAL GROSS WEIGHT 1,470 99.7 146,576
AP PROVED AFT LIMIT 101 INCHES
Sam ple based on sin gle 33 gal lon 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 2 of 2)
SCHWEIZER
Model 269C-1 Helicopter
CSP book 2..indd 128 8/4/19 12:53 PM
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