Performance - ATPL - Airline Transport Pilot license

Test 10 Questions ATPL - Airline Transport Pilot license - Performance, no time limit

1 - Which combination of circumstances or conditions would most likely lead to a tyre speed limited take-off? A high runway elevation and tail wind A low runway elevation and a head wind A high runway elevation and a head wind A low runway elevation and a cross wind

2 - If the aircraft mass, in a horizontal unaccelerated flight, decreases: The minimum drag increases and the IAS for minimum drag increases The minimum drag increases and the IAS for minimum drag decreases The minimum drag decreases and the IAS for minimum drag increases The minimum drag decreases and the IAS for minimum drag decreases

3 - With regard to the drift down performance of the twin jet aeroplane, why does the curve representing 35000 kg gross mass in the chart for drift down net profiles start at approximately 4 minutes at FL370? Due to higher TAS at this mass it takes more time to develop the optimal rate of descent, because of the inertia involved Because at this mass the engines slow down at a slower rate after failure, there is still some thrust left during four minutes All the curves start at the same point, which is situated outside the chart Because at this mass it takes approximately 4 minutes to decelerate to the optimum speed for drift down at the original cruising level[see Annex]

4 - If the take-off mass of an aeroplane is brake energy limited a higher uphill slope would: Decrease the maximum mass for take-off Increase the maximum mass for take-off Decrease the required take-off distance Have no effect on the maximum mass for take-off

5 - Maximum Tyre Speed can limit the Lift-off Speed.Which kind of speed can be directly used to determine this limitation? Groundspeed EAS TAS IAS

6 - In straight horizontal steady flight, at speeds below that for minimum drag: A lower speed requires a higher thrust. The aeroplane cannot be controlled manually. A higher speed, but still below that for minimum drag, requires a higher thrust. The aeroplane can be controlled only in level flight.

7 - To minimize the risk of hydroplaning during landing the pilot should: Use maximum reverse thrust, and should start braking below the hydroplaning speed. Use normal landing-, braking- and reverse technique. Make a 'positive' landing and apply maximum reverse thrust and brakes as quickly as possible. Postpone the landing until the risk of hydroplaning no longer exists.

8 - In case of an engine failure recognized below V1: The take-off must be rejected The take-off is to be continued unless V1 is less than the balanced V1 The take-off should only be rejected if a stopway is available The take-off may be continued if a clearway is available

9 - The drift down requirements are based on: The obstacle clearance during a descent to the new cruising altitude if an engine has failed The landing mass limit at the alternate The maximum flight path gradient during the descent The actual engine thrust output at the altitude of engine failure

10 - Considering TAS for maximum range and maximum endurance, other factors remaining constant: Both will stay constant regardless of altitude Both will decrease with increasing altitude TAS for maximum range will increase with increased altitude while TAS for maximum endurance will decrease with increased altitude Both will increase with increasing altitude

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