Exam quiz ATPL - Airline Transport Pilot license

Test 10 Questions atpl, no time limit

1 - Under what runway conditions is the braking action reported to be 'Unreliable': Runway covered with wet snow and slush Runway conditions normal Runway covered with dry snow Runway covered with ice

2 - An isohypse (contour) Indicates the true altitude of a pressure level Indicates the altitude of the zero degree isotherm Is the limit between two air masses of different temperature Is the longest slope line of a frontal surface

3 - The 'Black hole' phenomenon occurs during approaches at night and over water, jungle or desert. When the pilot is lacking visual cues other than those of the aerodrome there is an illusion of Being too close, landing long Climbing Being too high and too far away, dropping low and landing short Being too low, flying a steeper approach than normal

4 - The choice of the moment you select flaps depending on situation and conditions of the landing is: Knowledge based behaviour Skill and/or rule based behaviour Automated behaviour Pressure based behaviour

5 - Given: true course (TC) 017 W/V 340/30 TAS 420 kt Find: wind correction angle (WCA) and ground speed (GS) WCA +2° GS 396 kt WCA -2° GS 426 kt WCA -2° GS 396 kt WCA +2° GS 416 kt

6 - The location of the centre of pressure of a positive cambered wing at increasing angle of attack will: Not shift Shift forward Shift in spanwise direction Shift aft

7 - General provisions for ATS - obstacle clearanceWhen does Air Traffic Control Services have the responsibility to prevent collisions with terrain? Always when ATS are provided. When a flight in accordance with IFR is vectored by radar. ATS only provides prevention when an aircraft is flying IFR in IM ATS never prevent collisions with terrain.

8 - For a particular aeroplane, the structural maximum mass without any fuel on board, other than unusable quantities, is: A variable value which is governed by the payload carried. A fixed value which is stated in the Aeroplane Operating Manual. A fixed value which will limit the amount of fuel carried. A variable value which may limit the payload carried.

9 - Given:Pt: total pressure Ps: static pressurePd: dynamic pressure The altimeter is fed by: Ps-Pt Ps Pd-Ps Pd

10 - A climb gradient required is 3.3%. For an aircraft maintaining 100 KT true airspeed, no wind, this climb gradient corresponds to a rate of climb of approximately: 3 300 fpm 330 fpm 33.0 m/s 3.30 m/s

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