BRISTELL S-LSA - Loaded Aircraft Weight and CG

6-5
Date of Issue: 01/2016
Document No.: LSA-AOI-2-1-0-CL
Revision: -
6.2.1.2 Loaded Aircraft Weight and CG
ITEM
EMPTY AIRCRAFT
PILOT
PASSENGER
BAGGAGE - BEHIND
SEATS
BAGGAGE - FRONT
optional)
BAGGAGE - WING
LOCKERS
FUEL TANKS
CENTER OF GRAVITY
CG (mm)=
TOW= CG (%MAC) =
MT=
Max.Takeoff Weight: 600 kg Serial No.: 317/218
CG Range: 25 35 Date:
Forward limit: 337,5 mm By:
Rearward limit: 472,5 mm
LOADED ACFT TOTAL MOMENT
(kg.mm)
353,8
424,12
150054,4
LOADED AIRCRAFT
WEIGHT AND CG
600,0
600,0
1400,0
-300,0
630,0
200,0
LOADED AIRCRAFT
TAKEOFF WEIGHT
(kg)
WEIGHT
(kg)
ARM
(mm)
MOMENT = WEIGHT x ARM
(kg.mm)
MAC
x
100
(mm) CG (%MAC) CG 
Weight Total
Moment Total
(mm) CG 