Cessna 402C Pilot Operating Handbook page 201

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
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