EX AM PLE I - Based on 32.5 gal lon use able fuel
*Fuel CG is 108.5 for S/N 1743, 1744, 1746 and sub se quent.
Fuel CG is 107.0 for S/N 004 thru 1742 and 1745.
Cal cu la tion of Lon gi tu di nal CG
CG (Zero Fuel Weight):
Mo ment at Zero Fuel Weight 155,551
———————————— = ————— = 95.0 in.
Zero Fuel Weight
1,637
CG (Gross Weight):
Mo ment at Gross Weight 176,709
—————————— = ———— = 96.5 in.
Gross Weight 1,832
Note:
The CG’s fall within the lim its spec i fied in Fig -
ure 6-6; there fore, the load ing meets the lon gi tu di nal
CG re quire ments, for full fuel as well as zero fuel.
Weight and Balance
Pilot's Flight Manual
Reissued:
16 Jan 2019
6-9
Items
Weight
(lb)
Longitudinal
Moment
(in.-lb.)
De livered Weight
Pi lot - Left-Hand
Pas sen ger - Right-Hand
Pas sen ger - Cen ter
1. Sub-Total Gross Weight
Fuel
2. Gross Weight
1,127
113,663
170
170
170
1,637
195
14,144
14,144
13,600
155,551
21,158*
1,832
176,709
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 145
8/4/19 12:46 PM
Содержание S300C 269C
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