BEECHCRAFT Bonanza
V35, V35A & V35B thru D-9947
Section VI
Wt and Bal/Equip List
SAMPLE LOADING, V35B
5-Place Family Loading
(Within Flight C.G. Limits)
ARM
Item Weight (C.G.**)
Basic Empty Weight*** 2230 82.1
Occupant - Front (1) 87.0
82.4
Occupant - Front (1) 87.0
2550 82.7
Occupant - Cent
100 123.0
2650 84.2
Occupant - Center (1) 90 123.0
2740
85.5
Occupant - 5th (1)*
10
154.0
2750
85.7
MOM/100**
1830
165
1995
113
2108 ·
123
2231
111
2342
15
2357
• Enter weight, C.G., MOM/100 for this seat only if your airplane
is so occupied.
• • 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 .
. \JOTE: The 10 pound 5th occupant is the most that can be carried
in conjunction with the other occupant weights and keep the air-
plane C.G. within the aft C.G. limit.
March, 1987
6-141
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