Cessna 402B 1973 - Page 57

MODEL
4O2E
UTILILIN
E
R
SAMPLE
PROBLEM
Sample
Aircra-ft Your
Aircraft
Weight
(rbs)
Moment
(lb.
-ins.
/7000)
Weight
(lbs)
Moment
(lb.
-ins.
/7000)
1. Licensed
Empty
Weight
(Sample
Aircra-tt)
3973.
7
607.
I
2.
Oil
x(26
Qts.
x 1. 875 Lb/qt.
)
49.0
5.6
49.0
5.6
3.
Seat 1
and
Seat
2
340.0
46. 6
4.
Seat
3 and
Seat
4
340.0
56. 4
5.
Seat 5
and
Seat 6 340.0
65. 6
6,.
Seat 7 and Seat 8' 340.0 74.8
7. Seat 9 and
Seat
10
170. 0
42.0
8'
Fuet
(gals.
x
6 lbs.
/eaL)
Main
Tanks
(100
gafs.
)
Auxiliary
Wing Tanks
(20
gals.)
Wing Locker
Tanks
(20
Safs.)
600.0
91.2
v.
Eaggage
Nose
Cabin
Wing Lockers
107. 3
40.0
7.6
f . t
10. Cargo
A
B
C
D
11.
Total
AircraJt
Weight
(Loaded
6300.
0
1005.
1
t2.
Locate this
point(6300.0
at 1005. 1)on
Figure
4-6.
Since this
point
falls
within
the
envelope,
the loading is acceptable.
*Note:
Normallv full oil
mav
be
assumed
for
all fliehts.
Figure
4-4
4-8