test bank contains questions pertaining to
032-02-03 Elements of performance
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from the EASA ATPL
- The most efficient angle of attack is:
- If level flight is maintained but the air density decreases then this would cause:
- The speed for maximum lift/drag ratio will result in:
- When approaching a wet runway, with the risk of hydroplaning, what technique should the pilot adapt?
- Climbing to cruise altitude with a headwind will:
- Landing on a runway with 5mm wet snow will:
- The induced drag of an aeroplane:
- An aeroplane is in a power off glide at best gliding speed. If the pilot increases pitch attitude the glide distance:
- Which of the following combinations adversely affects take-off and initial climb performance?
- An aircraft is climbing at VX. If the speed is increased, maintaining the power setting,
- Which of the following statements is true regarding the performance of an aeroplane in level flight?
- Increased ambient temperature allows:
- The optimum altitude
- Calculate the still air gradient of climb, given that the aircraft climbs at 1500fpm with a TAS of 300kts and there is a tailwind of 50kts.
- The speed that will attain the greatest rate of climb is where the greatest excess of:
- If mass increases, the power required curve of an aeroplane:
- What happens to VX and VY as altitude increases?
- (CAP 698 figure 3.9)Find the maximum planned landing weight to comply with the regulations, for the following conditions:Pressure altitude: sea levelTemperature: 30° CForecast wind component: 10kt headRunway length: 3000ft (hard, dry and level)
- The pilot of a light twin engine aircraft has calculated a 4 000 m service ceiling, based on the forecast general conditions for the flight and a take-off mass of 3 250 kg. If the take-off mass is 3 000 kg, the service ceiling will be:
- The minimum total drag of an aircraft in level flight occurs:
- A FLAT RATED jet engine will give:
- Which of the following factors will lead to an increase of ground distance during a glide, while maintaining the appropriate minimum glide angle speed?
- If the runway is wet, the landing distance required for a dry runway:
- If the net gradient of climb after take-off with all engines operating is 14 percent in the prevailing conditions, the horizontal distance required to reach a height of 1500ft from the screen, if the cloud base is 2000ft, would be:
- For a turboprop powered aeroplane, a 2200 m long runway at the destination aerodrome is expected to be " wet" . The " dry runway" landing distance, should not exceed:
- For an aircraft flying in conditions that would give the balked landing climb limit gradient of 2.5 percent, the rate of climb that would be achieved at a TAS of 90kts would be:
- What is the effect of runway slope on take-off performance?
- What is the effect of increased mass on the maximum rate of climb speed (all other factors considered unchanged)?
- The speed instability region is:
- Which of the following statements is true with respect to the take-off flight path (multi engine class B)?
- Considering a turbine powered aircraft, when passing 35 feet at the end of the take-off distance, the speed should not be less than
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