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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
Using PFP-053e and fuel density 0.72 kg/L, what is the loaded CG arm including all listed fuel, rounded to 0.1 cm?
The calculated take-off mass is 750 kg and the total moment is 625 000 kg mm (equivalent to 625 kg m). Which numbered cross represents this loading? Use figure (PFP-003); its metric horizontal scale is moment divided by 1 000.
The calculated take-off mass is 725 kg and the total moment is 650 000 kg mm (equivalent to 650 kg m). Which numbered cross represents this loading? Use figure (PFP-004); its metric horizontal scale is moment divided by 1 000.
The calculated take-off mass is 775 kg and the total moment is 700 000 kg mm (equivalent to 700 kg m). Which numbered cross represents this loading? Use figure (PFP-005); its metric horizontal scale is moment divided by 1 000.
Using figure (PFP-006), calculate the empty mass and centre-of-gravity arm after all three equipment changes. Round the CG arm to three decimal places.
How does the aircraft configuration influence take-off performance while all other parameters remaining constant? See figure (PFP-007)
In a typical light aeroplane, increasing flaps within the approved take-off settings can have which effects, with other factors unchanged?
How does wind affect the take-off performance?
During initial climb, the aeroplane passes from a sheltered weak tailwind into a stronger tailwind aloft. Without correction, what immediate effect may occur?
Which factor shortens landing distance?
