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EN Flight Performance and Planning - EASA PPL(A) - Private Pilot Licence (Aeroplane)
Questions Flight Performance and Planning - EASA PPL(A) aeroplane theory
Empty mass is 540 kg at arm 0.40 m. Load is 90 kg at arm 1.10 m. What is the loaded centre of gravity? Use one common datum for all arms and round to the nearest 0.01 m.
Empty mass is 800 kg at arm 0.30 m. Load is 150 kg at arm 0.75 m. What is the loaded centre of gravity? Use one common datum for all arms and round to the nearest 0.01 m.
Empty mass is 650 kg at arm 0.28 m. Load is 200 kg at arm 0.95 m. What is the loaded centre of gravity? Use one common datum for all arms and round to the nearest 0.01 m.
Total mass is 750 kg and total moment is 285.0 kg m. What is the centre of gravity arm? Use one common datum for all arms and round to the nearest 0.01 m.
Total mass is 820 kg and total moment is 311.6 kg m. What is the centre of gravity arm? Use one common datum for all arms and round to the nearest 0.01 m.
Total mass is 900 kg and total moment is 360.0 kg m. What is the centre of gravity arm? Use one common datum for all arms and round to the nearest 0.01 m.
Total mass is 680 kg and total moment is 272.0 kg m. What is the centre of gravity arm? Use one common datum for all arms and round to the nearest 0.01 m.
Total mass is 1040 kg and total moment is 416.0 kg m. What is the centre of gravity arm? Use one common datum for all arms and round to the nearest 0.01 m.
For an arithmetic exercise, multiply a distance of 450 m by the specified factor 1.15. What is the result rounded to the nearest metre? This exercise factor is not a universal operational correction; real planning uses the applicable AFM/POH.
For an arithmetic exercise, multiply a distance of 520 m by the specified factor 1.20. What is the result rounded to the nearest metre? This exercise factor is not a universal operational correction; real planning uses the applicable AFM/POH.
