Section VI BEECHCRAFT Bonanza
Wt and Bal/Equip List V35, V35A & V35B thru D-9947
SAMPLE LOADING, V35B
&-Place Family Loadings
(Within Flight C.G. Limits)
ARM
Item Weight (C.G.**) MOM/100**
Basic Empty Weight•••
Occupant - Front (1)
Occupant - Front (1)
Occupant - Center (1)
Occupant - Center (1)
Occupant - 5th (1)*
Occupant - 6th ( 1)'
2230 82.1
190 87.0
50 123.0
2650 84.5
25 154.0
2675
85.1
23 154.0
2698 85.7
1830
165
1995
96
2091
86
2177
62
2239
38
2277
35
2312
• Enter weight, C.G., MOM/100 for these seats only if your air-
plane 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.
6-14J
NO fE: 23 pounds is all that can be carried on the 6th seat without
the airplane C.G. exceeding the aft C.G. limit.
March, 1987
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