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from the EASA ATPL
- All other factors being equal minimum drag speed is...
- What is a COST INDEX?
- Which of the following variables will not affect the shape or position of the drag-IAS curve, for speeds below Mcrit:
- What is the effect of the centre of gravity on fuel consumption?
- Equivalent airspeed is equal to:
- If the thrust available exceeds the thrust required for level flight:
- A twin jet aeroplane is in cruise, with one engine inoperative, and has to overfly a high terrain area. In order to allow the greatest clearance height, the appropriate airspeed must be the airspeed
- Buffet may occur :
- The maximum speed that can be achieved in level flight will occur :
- With all other things remaining unchanged and with T the outside static air temperature expressed in degrees K, the hourly fuel consumption of a turbojet powered aeroplane in a cruise flight with a constant Mach Number and zero headwind, is as follows:
- During a driftdown following engine failure, what would be the correct procedure to follow?
- The speed range between low speed buffet and high speed buffet
- For a non-ETOPs approved twin engine aircraft:
- ETOPS flight is a twin engine jet aeroplane flight conducted over a route, where no suitable airport is within an area of:
- For an aircraft cruising at a constant altitude and a constant angle of attack, as weight decreases :
- The optimum cruise altitude increases:
- The effect of flying at the Long Range Cruise speed instead of the Maximum Range Cruise speed is:
- Which of the following statements is correct with regard to increasing altitude?
- The optimum cruise altitude is:
- At maximum range speed in a turbojet the angle of attack is:
- The speed for minimum power in a turbojet will be:
- The tangent from the origin to the Drag-Speed curve will give, for a jet aircraft, the speed for:
- If the calculations for an aeroplane of 3250lb indicate a service ceiling of 4000m. What will the service ceiling be for an aircraft with a weight of 3000lb?
- A jet aeroplane is flying long range cruise. How does the specific range / fuel flow change?
- To obtain the maximum range for a jet aircraft it should be flown:
- Which of the following parameters have an influence on high-speed buffeting?
- The airspeed for jet aeroplanes at which power required is a minimum:
- With zero wind, the angle of attack for maximum range for an aeroplane with turbojet engines is:
- Two identical turbojet aeroplane (whose specific fuel consumptions are considered to be equal) are at holding speed at the same altitude.The mass of the first aircraft is 130 000 kg and its hourly fuel consumption is 4300 kg/h. The mass of the second aircraft is 115 000 kg and its hourly fuel consumption is:
- 'Drift down' is the procedure to be applied:
- Which data can be extracted from the Buffet Onset Boundary Chart?
- Given a constant altitude. If the mass of a jet aeroplane is increased by 5% and assuming the engine specific fuel consumption remains constant, the hourly fuel consumption increases by approximately:
- The pilot of a jet aeroplane wants to use a minimum amount of fuel between two airfields. Which flight procedure should the pilot fly?
- (Refer to CAP 698 Figure 4.5)PMC is the:
- An aircraft with 180 minutes ETOPS approval must be:
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