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EN ATPL Performance Questions in English
Practise Performance
Assuming both flight levels are permitted by all aircraft and operational limits, which wind condition could make cruising 4000 ft or more below the still-air optimum altitude more fuel-efficient over the ground, if the wind benefit outweighs the lower-altitude fuel penalty?
The drift down procedure specifies requirements concerning the:
In the quasi-steady descent approximation, an aeroplane descends from FL410 to FL270 at constant Mach, then to FL100 at constant IAS. Assume fixed mass and clean configuration, negligible idle thrust and kinetic-energy corrections, incompressible flow, and flight on the high-speed side of minimum drag. How does the descent angle change in the first and second parts?
The induced drag of an aeroplane:
What will be the influence on the aeroplane performance if aerodrome pressure altitude is increased?
An increase in atmospheric pressure has, among other things, the following consequences on take-off performance:
On a reciprocating engine aeroplane, with increasing altitude at constant gross mass, angle of attack and configuration the power required:
The speed V1 is defined as:
Which of the following combinations adversely affects take-off and initial climb performance?
For the fictional MEP1 aeroplane in CAA CAP698, using the prescribed surface and slope corrections on a dry runway, which of the following increases the calculated accelerate-stop distance?
Other exam subjects ATPL - Airline Transport Pilot Licence
- Air Law
- Aircraft General Knowledge - Airframe, Systems, Powerplant
- Aircraft General Knowledge - Instrumentation
- Communications
- Flight Planning and Monitoring
- General Navigation
- Human Performance and Limitations
- Mass and Balance
- Meteorology
- Operational Procedures
- Principles of Flight
- Radio Navigation
