Section VI
Wt and Bal/Equip List
BEECHCRAFT Bonanza
V35, V35A & V35B thru D-9947
SAMPLE LOADING, V35B
5-Place Family Loadings
(Outside Flight C.G. limits)
ARM
Item Weight (C.G.**)
Basic Empty Weight* ..
Occupant - Front ( 1)
85.1
Occupant - 5th (1)*
60
154.0
2750 86.5
Baggage
100 150.0
2850 88.8
MOM/100**
165
96
111
2202
86
2288
92
2380
150
2530
• 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: Loading 100 pounds of baggage and a 60 pound 5th occu-
pant places the airplane C.G. 3.1 inches outside the aft C.G. limit. To
correct this problem, remove all the baggage and reduce the 5th oc-
cupant weight to 25 pounds.
6-14H March, 1987
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