Section VI
Wt and Bal/Equip List
BEECHCRAFT Bonanza
V35, V35A & V35B thru D-9947
SAMPLE LOADING, V35, V35A
5-Place Family Loading
(Within Flight C.G. Limits)
ARM
Item Weight (C.G.
0
) MOM/100°
Basic Empty Weight*• *
Occupant - Front ( 1)
Occupant - Front (1)
Occupant - Center (1)
Occupant - Center (1)
Occupant - 5th ( 1) *
Baggage
2092
79.8
90 123.0
2602 83.9
60 154.0
2662 85.4
11 150.0
2673 85.7
1670
165
1835
113
1948
123
2071
111
2182
92
2274
16
2290
• 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.
NOTE: The 11 pounds of baggage was calculated to place the air-
plane C.G. on the aft C.G. limit. Additional baggage will cause the
airplane C.G. to exceed the aft C.G. limit.
6-14D
March, 1987
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