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EN ATPL Performance Questions in English
Practise Performance
Which combination of circumstances or conditions would most likely lead to a tyre speed limited take-off?
The minimum climb gradient required on the 2nd flight path segment after the take-off of a jet aeroplane is defined by the following parameters: 1. Gear up 2. Gear down 3. Wing flaps retracted 4. Wing flaps in take-off position 5. N engines at the take-off thrust 6. (N- 1) engines at the take-off thrust 7. Speed over the path equal to V2 + 10 kt 8. Speed over the path equal to 1.3 VS 9. Speed over the path equal to V2 10. At a height of 35 ft above the runway. The correct statements are:
Regarding the obstacle limited take-off mass, which of the following statements is correct?
The take-off mass of an aeroplane is restricted by the climb limit. What would be the effect on this limit of an increase in the headwind component?
For a jet aeroplane, in the simplified model where available thrust is approximately constant with airspeed, maximum climb angle in still air occurs at the speed corresponding to:
As long as an aeroplane is in a positive climb:
Two identical turbojet aeroplanes (whose specific fuel consumptions are considered to be equal) are at holding speed at the same altitude. The mass of the first aircraft is 130000 kg and its hourly fuel consumption is 4300 kg/h. The mass of the second aircraft is 115000 kg and its hourly fuel consumption is:
Which data can be extracted from buffet onset boundary data?
In the fictional MRJT1 drift-down profiles in CAA CAP698, when using the standard bleed configuration and considering only the temperature correction, what does equivalent gross mass at engine failure represent?
The intersections of the thrust available and the drag curve are the operating points of the aeroplane
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
