Beech Beechcraft Bonanza V35 Pilot Operating Handbook page 149

BEECHCRAFT Bonanza
V35, V35A & V35B thru D-9947
Section VI
Wt and Bal/Equip List
SAMPLE LOADING, V35, V35A
5-Place Family Loading
(Outside Flight C.G. Limits)
ARM
Item Weight (C.G.**
Basic Empty Weight*•• 2092 1670
-----------------
0 c cup ant - F ront ( 1)
165
Occupant - I ·ont (1)
Occupant- 60
2662
Baggage 150
2812
123.0
83.9
154.0
85.4
150.0
88.9
1835
113
1948
123
2071
111
2182
92
2274
225
2499
• 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 tor 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 tor
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 baggage (30 lb. per occupant) placed the airplane
C.G. 3.2 inches outside the flight C.G. limit. To correct this problem
139 pounds of baggage must be removed.
March, 1987 &-14C