BRISTELL S-LSA - Weight and CG Blank Form

6-6
Date of Issue: 01/2016
Document No.: LSA-AOI-2-1-0-CL
Revision: -
6.2.1.3 Weight and CG Blank Form
ITEM
RIGHT MAIN WHEEL WR= LR= 720,0 MR=
LEFT MAIN WHEEL WL= LL= 720,0 ML=
NOSE WHEEL WN= LN= -750,0 MN=
CG (mm) =
WE= CG (%MAC) =
MT=
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
Max.useful load:
WU (kg) = MTOW - WE
WU (kg) = 600 -
WU (kg) =
WARNING
DO NOT EXCEED MAXIMUM TAKEOFF WEIGHT 600 kg!
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)
EMPTY AIRCRAFT
WEIGHT AND CG
EMPTY AIRCRAFT
EMPTY WEIGHT
(kg)
EMPTY ACFT TOTAL MOMENT
(kg.mm)
WEIGHT
(kg)
ARM
(mm)
MOMENT = WEIGHT x ARM
(kg.mm)
LOADED ACFT TOTAL MOMENT
(kg.mm)
MAC
x
100
(mm) CG (%MAC) CG 
Weight Total
Moment Total
(mm) CG 