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Cessna 402C - Page 201

Cessna 402C
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C'~402C
MODEL
SECTION
6
WEIGHT
&
BALANCE
--
WEIGHT
AND
BALANCE
FORM
BUSINESSLINER
AND
UTlLlLlNER PASSENGER
CONFIGURATION
R
PAYLOAD
COMPUTATIONS
E
ITEM
WEIGHT
MOMENT/
F
100
ITEM
I.
BASIC
EMPTY
OCCUPANTS
ARM
WEIGHT
MOMENT/
WEIGHT
OR
CARGO
IDD
2.
PAYLOAD
SEAT
1
3.
ZERO
FUEL
WEIGHT
SEAT
(sub-total)
(Do
-
not exceed
maximum
SEAT
-
zero fuel weight
SEAT
of
6515
pounds)
-
4.
FUEL
LOADING
SEAT
-
5.
RAMP
WEIGHT
SEAT
-
(sub-total)
(Do
not exceed
maximum
SEAT
ramp
weight
of
-
6885
pounds)
SEAT
-
6.
LESS
FUEL
FOR
SEAT
-
TAXIING
SEAT
-
7.
TAKEOFF
WEIGHT
(Do
not
exceed
TOILET
maximum
takeoff
weight of
6850
BAGGAGE
pounds)
WING
8.
LESS
FUEL
TO
LOCKERS
DESTINATION
AVIONICS
9.
LANDING
WEIGHT
(Do
not exceed
NOSE
maximum
landing
weight of
6850
BAY
A
pounds)
BAY
B
CABINET
CONTENTS
PAYLOAD
Totals
must
be
within
approved weight
and
C.G.
limits.
It;s
the
responsi-
bility
of
the operator to insure that the airplane
is
loaded properly.
The
Bas;c
Empty
Weight
e.G.
is
noted
on
the Airplane
Weighing
Form.
If
the
airplane
has
been
altered,
refer
to the
Weight
and
Balance
Record
for
this
information.
1
November
1979
6-53/6-54

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