EASA 031 Mass & Balance case studies
EASA 031 Mass & Balance · Put your knowledge to work in context.
Mass & Balance (031) is one of the knowledge modules required for EASA Part-66 aircraft maintenance licences, and it also underpins the theoretical knowledge expected of pilots and dispatchers. It tests whether you can work confidently with aircraft mass, centre of gravity and the documentation that controls both. The subject is deliberately practical: you are asked to convert between mass and weight, identify which structural or performance limit governs a given flight, compute moments and CG positions from loading data, and explain why a forward or aft CG affects stability, control and fuel consumption. Candidates meet it in both maintenance and flight-training pathways, so the syllabus ranges from definitions and weighing procedures to hold loading limits, load sheets and fuel density corrections. The EASA 031 Mass & Balance case studies are 5 cases and about 2,233 words.
1Fuel burn pulls the CG forward
A twin-engine turboprop is dispatched at a take-off mass of 5,000 kg with a CG at 4.50 m aft of the datum. The forward CG limit is 4.40 m and the aft limit is 5.05 m.
471 words, about 2 min2Which limit actually stops the take-off?
A regional twin-jet has BEM 3,620 kg at 4.10 m. Crew 220 kg at 2.50 m; removable service equipment 80 kg at 3.00 m.
404 words, about 2 min3Three-scale weighing after a modification
After a repaint and interior modification, a light twin is weighed in a level hangar. The aircraft is prepared with unusable fuel, full oil and coolant, no payload, and doors closed.
448 words, about 2 min4Aft hold floor limit and aft CG together
An aircraft is being loaded for a cargo flight. Before cargo, mass is 4,650 kg and CG is 4.68 m; aft CG limit is 5.02 m.
421 words, about 2 min5Fuel density changes the mass, not the litres
Before a short flight, a piston twin has a basic empty mass of 2,950 kg at 3.95 m; this figure already includes full oil and 10 L of unusable fuel. Pilot and front passenger weigh 170 kg at 2.40 m; baggage is 30 kg at 5.20 m.
489 words, about 2 min