BEECHCRAFT Bonanza
V35, V35A & V35B thru D-9947
Section VI
Wt and Bal/Equip List
Item
SAMPLE LOADING, V35B
Four 190-Pound Occupants
(Outside Flight C.G. Limits)
ARM
Basic Empty Weight*•
Occupant - Front (1)
85.5
Occupant 190 123.0
2990 87.9
1830
165
1995
165
2160
234
2394
234
2628
• Use the C.G., MOM/100 for the occupants as they are posi-
tioned in your airplane. Consult the POH Weight and Balance
Section for the latest occupant positions. If the seats are ad-
justable fore and aft, use the position in which that seat is locat-
ed during flight.
The Basic Empty Weight Data shall be current and accurate for
the airplane as equipped. ·
NOTE: The addition of fuel to the above loading will move the cen-
ter of gravity (C.G.) forward. Conversely, using fuel during flight will
move the airplane center of gravity aft. Flight safety requires that
during flight the airplane weight and center of gravity be within the
approved limits.
NOTE: Four 190-pound occupants cannot be loaded and remain
within the aft C.G. limit of F.S. 85.7. 175 pounds must be reduced in
one center seat to place the airplane C.G. on the aft C.G. limit.
March, 1987
6-14G
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