General Mass Calculations: Fuel Density, Standard Masses, and LMC

031-02-03Pablo Asensio Martínez2026-04-011 min

Calculating Total Mass

The total mass of the aircraft is the sum of all its components:

  1. Start with Basic Empty Mass (BEM).
  2. Add Crew and Pantry to get Dry Operating Mass (DOM).
  3. Add Traffic Load (Passengers + Bags + Cargo) to get Zero Fuel Mass (ZFM).
  4. Add Take-off Fuel to get Take-Off Mass (TOM).

Fuel Calculations

Fuel is often measured in volume (Litres or US Gallons) but must be converted to mass (kg or lbs) for weight and balance calculations.

  • Formula: $\text{Mass} = \text{Volume} \times \text{Density (SG)}$
  • Specific Gravity (SG): The ratio of the density of the fuel to the density of water.
    • Jet A-1 SG $\approx 0.8$ (ranges 0.78 - 0.84).
    • Avgas SG $\approx 0.72$.

Example: 1000 Litres of Jet A-1 at SG 0.8 $ \text{Mass} = 1000 \times 0.8 = 800 \text{ kg} $

Passenger Mass

For large aircraft, standard masses are often used for passengers and baggage to simplify calculations, rather than weighing each individual.

  • Standard Mass: A statistical average value set by the authority (e.g., EASA) which includes hand baggage.
  • Actual Mass: Used when standard masses are not applicable (e.g., small aircraft with fewer than 10 seats, or non-standard flights).

Adjustments

Always account for:

  • Last Minute Changes (LMC): Additions or removals of passengers/cargo after the load sheet is finalized.
  • Total mass must be recalculated to ensure limits are not exceeded.
Written and reviewed by

Pablo Asensio

Aeronautical engineer. Passed the thirteen EASA ATPL(A) theoretical knowledge exams studying from these very notes. Writes and reviews each topic against the Part-FCL Learning Objectives.