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
6-10
Blank form of Loading and C.G. check
WEIGHT & BALANCE RECORD
Aircraft C.G. check table
ITEM
WEIGHT
lb
ARM
in
MOMENT
lb in
EMPTY AIRCRAFT
PILOT
27.56
PASSENGER
27.56
BAGGAGE
COMPARTMENT
51.58
WING LOCKERS
23.62
FUEL TANKS
7.09
TOTAL
W
T
=
C.G.
=
in
% MAC
M
T
=
NOTE:
Empty weight is including oil, coolant, hydraulic fluid and unusable fuel.
Maximum fuel quantity in wing tanks (30.1 US gal = 180.6 lb) is used for most forward C.G.
calculation.
Zero fuel quantity in wing tanks is used for most rearward C.G. calculation (in case of total fuel
depletion).
Max. takeoff weight :
1,320 lb
Max. weight in baggage compartment :
40 lb
Max. weight in each wing locker :
22 lb
Empty weight C.G. range :
16.83 to 17.42 in / 28.5 to 29.5 % of MAC
Operating C.G. range :
16.54 to 20.67 in / 28 to 35 % of MAC
MAC :
59.06 in
MOMENT (lb in) = WEIGHT (lb) x ARM (in)
M
T
100
AIRCRAFT C.G. = ------- (in) x -------- (%) of MAC
W
T
MAC
Registration:
Serial No.:
Date:
By:
