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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
What is the required distance to climb from FL 65 to FL 95 under the following conditions: Aircraft mass: 3000 lb. OAT in FL 65: -5° C OAT in FL 95: -15° C See annex (PFP-023)
What is the required distance to climb to flight level (FL) 75 after a departure from an airfield which is located at a pressure altitude of 3000 ft with an initial mass of 3000 lbs? OAT at airfield: 25° C OAT in FL 75: 0° C See annex (PFP-023)
On a chart using 30-minute latitude/longitude quadrangles, what does the maximum elevation figure (MEF) represent?
What is the purpose of a readily identifiable catching feature or limit line in visual navigation?
The VFR semicircular rules are based on the...
For true course 181° and variation 3°E, which of the listed flight levels fits the standard eastbound VFR semicircular allocation, assuming flight levels and that allocation are applicable?
The upper limit of LO R 16 equals... See annex (PFP-056)
The upper limit of LO R 4 equals... See annex (PFP-030)
Actual ramp mass is 1148 kg and maximum take-off mass is 1145 kg. Using fuel density 0.72 kg/L, what minimum fuel volume must be burned before take-off, rounded upwards to 0.1 L?
Considering the following fuel data, how much trip fuel is required? Fuel for start-up and taxi: 5 L Fuel for take-off and climb: 12 L Fuel for cruise flight: 25 L Fuel for descent, approach and landing: 7 L Fuel for taxi and parking: 3 L Fuel to alternate: 13 L Final reserve fuel: 10 L
