SC-POH-1-1-17
SECTION 6
WEIGHT & BALANCE
Revision: -
Date of issue: 2011-09-01
S
S
p
p
o
o
r
r
t
t
C
C
r
r
u
u
i
i
s
s
e
e
r
r
6-9
Loading and C.G. check table – zero fuel
ITEM
WEIGHT
lb
ARM
in
MOMENT
lb in
EMPTY AIRCRAFT
851.4
17.02
14,493.06
PILOT
187.0
27.56
5,153.72
PASSENGER
143.0
27.56
3,941.08
BAGGAGE
COMPARTMENT
22.0
51.58
1,134.76
WING LOCKERS
22.0
23.62
519.64
FUEL TANKS
0.0
7.09
0.0
TOTAL
W
T
=
1,225.4
C.G.
=
19.63
in
33.2
% MAC
M
T
=
25,242.26
4-6
Date of Issue: 12/2007
Revision: 2.0
WEIGHT & BALANCE REPORT
Forward CG Check
WEIGHT
[lb]
ARM
[in]
MOMENT
(WEIGHT x ARM)
EMPTY AIRCRAFT
842.3
--------
14 450.0
PILOT
88.0
27.6
2 428.8
PASSENGER
0
27.6
0
BAGGAGE
COMPARTMENT - A
0
51.6
0
BAGGAGE
COMPARTMENT - B
0
70.9
0
WING LOCKERS
0
23.6
0
FUEL TANKS
181.0
7.1
1 285.1
TOTAL
W
T
=
1 111.3
[lb]
M
T
=
18 163.9
TAKE-OFF WEIGHT 1 111.3
[lb]
CG
=
16.3
[in]
27.7
% MAC
Max. take-off weight :
1 320 [lb]
Max. weight in baggage compartment A+B :
40 [lb]
Max. weight in wing lockers together :
88 [lb]
Operating CG range :
27 to 38 % of MAC
M
T
100
Aircraft CG
= -------- [ in ] x --------- [ % ]
W
T
MAC
