Weight & Balance

Create aircraft profiles locally and compute CG visually. Data is saved in your browser only.

Profile

Name

Weight unit Arm unit

Basic Empty Weight (kg) Empty CG arm (mm)

Front seats arm (mm) Rear seats arm (mm) Fuel arm (mm) Baggage 1 arm (mm) Baggage 2 arm (mm) Fuel density (kg/L)

Max takeoff weight (kg)

Simple CG limits (mm)

If you don't use detailed envelope below, these will be applied.

Detailed envelope (optional) — one per line: weight,minCG,maxCG

Used for interpolation of min/max CG at the calculated weight.

Load case

Front seats total (kg) Rear seats total (kg) Baggage 1 (kg) Baggage 2 (kg) Fuel amount (L)

Fuel weight = amount × density

Calculating…

Total W: –

Total M: –

CG: –

Status: –

Envelope