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
6-8
Example of Loading and C.G. check
Aircraft empty data:
weight ..................................
851.4 lb
arm ......................................
17.02 in
moment ...............................
14,493.06 lb in
MAC ....................................
59.06 in
Operating weights:
pilot .....................................
187.0 lb
passenger ...........................
143.0 lb
baggage in cockpit ..............
22.0 lb
baggage in wing lockers ......
22.0 lb
fuel in tanks .........................
94.6 lb (15.8 US gal)
Loading and C.G. check table
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
94.6
7.09
670.71
TOTAL
W
T
=
1,320.0
C.G.
=
19.63
in
33.2
% MAC
M
T
=
25,912.98
4-7
Date of Issue: 12/2007
Revision: 2.0
WEIGHT & BALANCE REPORT
Rear CG Check
WEIGHT
[lb]
ARM
[in]
MOMENT
(WEIGHT x ARM)
EMPTY AIRCRAFT
842.3
--------
14 450.0
PILOT
190.0
27.6
5 244.0
PASSENGER
190.0
27.6
5 244.0
BAGGAGE
COMPARTMENT - A
33.0
51.6
1 702.8
BAGGAGE
COMPARTMENT - B
7.0
70.9
496.3
WING LOCKERS
27.0
23.6
637.2
FUEL TANKS
11.0
7.1
78.1
TOTAL
W
T
=
1 300.3
[lb]
M
T
=
27 852.4
TAKE-OFF WEIGHT 1 300.3
[lb]
CG
=
21.4
[in]
36.2
% 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
Serial No.:
08SC142
Date:
2008-04-23
By:
Otakar Hrabinec
