Weight & Balance
Load your aircraft, see the takeoff weight and centre of gravity, and check both against the certificated envelope for the category you are flying in - instantly. Under EASA it is called mass and balance; the sums are the same.
Non-aerobatic operations: normal flying, stalls except whip stalls, lazy eights, chandelles, and turns up to 60 degrees of bank.
Loaded result
Within limitsCessna 172S Skyhawk SP · Normal category · data checked 2026-10-12
The printed sheet carries the aircraft, the date, every station, all three points of the flight and the full safety notice - free, no sign-up, and it prints offline.
CG envelope
Takeoff and landing plotted against the Cessna 172S Skyhawk SP normal-category envelope.
- Normal envelope
- Takeoff
- Landing
- Fuel burning off
Each point is labelled IN or OUT, and both must sit inside the envelope.
The bar through the takeoff point is how far the CG slides as the adjustable seats run through their published travel: 40.65 to 42.45 in. Both ends stay inside the envelope.
Datum: the lower portion of the front face of the firewall. All arms are inches aft of that (POH Section 2, p. 2-7). Full limits and sources
Loading
Weights in pounds; fuel in US gallons. Arms are fixed by the airframe.
Illustrative only - a mid-range 172S basic empty weight and arm. It is not any real airframe. Replace both numbers from your aircraft W&B record.
POH Figure 6-3: occupant CG 37 in with the seats set for an average occupant, range 34 to 46 in over the seat travel.
Your rule sets it: under 14 CFR 91.151 (VFR), at least 30 minutes at normal cruising speed by day and 45 at night; the EASA and UK minutes are on the fuel reserves page.
Loadouts
Saved on this device only - a loadout is never sent to us.
Breakdown
Weight x arm = moment, per station.