Cessna 402C - Page 156

SECTION 6
WEIGHT & BALANCE
(M~,402C
SAMPLE WEIGHT AND BALANCE FORM
R
PAYLOAD COMPUTATIONS E
ITEM
WEIGHT MOMENT/
F
100
ITEM
1.
BAS IC EMPTY
OCCUPANTS
ARM WEIGHT
MDMENT/
WEIGHT 4225
6526.6
OR CARGO
100
2.
PAYLOAD IIlO
1820.0
SEAT I
137 170
233
3.
ZERO FUEL WEIGHT
SEAT 2 137 190
260
(sub-total) (Do
not exceed maximum
SEAT 3 175
100 175
zero fuel weight
of 6515 pounds) 5335
8346.6
SEAT 4 175 140
245
4.
FUEL LOADING
900
1455
SEAT 5 218
200 436
5.
RAMP WEIGHT
SEAT 6 218
200
436 (sub-total) (Do
not exceed maximum
SEAT
ramp weight of
-
6885 pounds) 6235 9801.6
SEAT
-
6.
LESS FUEL FOR
SEAT
TAXIING
35
58
-
SEAT
7.
TAKEOFF WEIGHT
-
(Do not exceed
TOILET
maximum takeoff
weight of 6850
BAGGAGE
pounds)
6200
9743.6
WING
8. LESS FUEL TO
LOCKERS
DESTINATION
628
1018.7
AVIONICS
g.
LANDING WEIGHT
(Do not exceed
NOSE
32
IlO
35
maximum landing
weight of 6850
BAY A
pounds)
5572
8724.9
BAY B
CABINET
CONTENTS
--
--- ---
PAYLOAD
--
lIlO 1820
Totals must be within approved weight and e.G. limits. It is the responsi-
bility of the operator to insure that the airplane is loaded properly. The
Basic Empty Weight C.G. is noted on the Airplane Weighing Form. If the
airplane has been altered, refer to the Weight and Balance Record for this
information.
Figure 6-3
1 NnvPmhpr lq7q
-.
-
-