Cessna 402C - Page 203

C<~, 402C
MODEL
SECTION 6
WEIGHT & BALANCE
WEIGHT AND BALANCE FORM
UTiLILINER CARGO CONFIGURATION
R
PAYLOAD COMPUTATIONS E
ITEM WEIGHT MOMENT/
F 100
ITEM I.
BASIC EMPTY
OCCUPANTS
ARM WEIGHT MOMENT/
WEIGHT
OR CARGO 100
2.
PAYLOAD
SEAT I
3.
2ERO FUEL WEIGHT
SEAT 2 (sub-total) (Do
not exceed maximum
BAGGAGE
zero fuel weight
of 6515 pounds)
WING
LOCKERS
4.
FUEL LOADING
AVIONICS
5.
RAMP WEIGHT
(sub-total) (Do
NOSE
not exceed maximum
ramp weight of
BAY A
6885 pounds)
BAY B
6.
LESS FUEL FOR
TAXIING
CARGO A
7.
TAKEOFF WEIGHT
CARGO B
(Do not exceed
maximum takeoff
CARGO C
weight
of 6B50
pounds)
CARGO D
8. LESS FUEL TO
CABINET
DESTINATION
CONTENTS
g.
LANDING WEIGHT
PAYLOAD
(Do not exceed
maximum landing
weight of 6B50
pounds)
Totals must be within approved weight and C.G. limits. It;s the responsi-
bility of the operator to insure that the airplane ;s loaded properly. The
Basic Empty Weight C.G. ;s noted on the Airplane Weighing Form. If the
airplane has been altered, refer to the Weight and Balance Record for this
information.
I November 1979
6-55/6-56