Schweizer S300C 269C - Page 148

Weight and Balance
Pilot's Flight Manual
6-12
Reissued: 16 Jan 2019
EX AM PLE II - Based on 32.5 use able gal lon fuel


Cal cu la tion of Lat eral CG:
   CG (Zero Fuel Weight):
Mo ment at Zero Fuel Weight +609
———————————— = ———— = + 0.4 in.
Zero Fuel Weight 1,637
   CG (Gross Weight):
Mo ment at Gross Weight + 4,002
—————————— = ———— = + 2.2 in.
Gross Weight 1,832
Note
: The de ter mined lat eral CGs of +0.4 inch and
+2.2 inch for lon gi tu di nal CGs of 95.0 inch and 96.5
inch re spec tively, fall within the es tab lished CG lim its.
(Ref er ence Fig ure 6-1 and Ex am ple I.)
Items
Weight
(lb)
Lateral
Moment
(in.-lb.)
Pi lot - Left-Hand
Pas sen ger - Right-Hand
Pas sen ger - Cen ter
1. Sub to tal Gross Weight
Fuel - Full Tank (32.5 use able gal)
2. New Gross Weight
170
170
170
- 2,346
+2,346
+128
1,637
195
+609
+3,393
1,832 + 4,002
De livered Weight
1,127 + 481
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 148 8/4/19 12:46 PM