BEECHCRAFT Bonanza Section VI
V35, V35A & V35B thru D-9947 Wt and Bal/Equip List
SAMPLE LOADING, V35, V35A
6-Place Family Loading
(Within Flight C.G. Limits)
ARM
Item
Weight
(C.G.**)
MOM/100**
Basic Empty Weight***
2092 79.8
1670
Occupant - Front (1)
190 87.0 165
2282
80.4
1835
Occupant - Front ( 1)
~7.0
113
"'-\\\I
80.8
1948
Occupant - Center(~~~\:
- 100
123.0
123
2512 82.4
2071
Occupant - Center (1) 90 123.0
111
2602 83.9
2182
Occupant - 5th (1)*
60
154.0 92
2662 85.4
2274
Occupant - 6th (1)* 11 154.0
17
2673
85.7
2291
• 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.
NOTE: 11 pounds is all that can be carried on the 6th seat without
the airplane C.G. exceeding the aft C.G. limit.
March, 1987 6-14E
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