Quiz di esame ATPL - Airline Transport Pilot license

Test 10 domande atpl, tempo libero

1 - Given:Pt = total pressure Ps = static pressure Dynamic pressure is: (Pt - Ps) / Ps (Pt - Ps) / Pt Pt / Ps Pt - Ps

2 - Within the Annex to the ICAO convention that specifies dimensions of aerodromes is a specific dimension given for the approach light system for CAT 1 ILS. What should be the length of this approach light system? 900 metres 1200 metres 1000 metres 420 metres

3 - An aircraft is flying at MACH 0.84 at FL 330. The static air temperature is -48°C and the headwind component 52 Kt. At 1338 UTC the controller requests the pilot to cross the meridian of 030W at 1500 UTC. Given the distance to go is 570 NM, the reduced MACH No. should be: 0.76 0.78 Given the distance to go is 570 NM, the reduced MACH No. should be: 0.76 0.78 0.72 0.80

4 - Refer to CAP697 Section 4 - MRJT1 Page 19 Figure 4.5.1 En-route Climb 280/0.74 Given: brake release mass 57500 kgtemperature ISA -10°C head wind component 16 KT initial FL 280Find: still air distance (NAM) and ground distance (NGM) for the climb 59 NAM 62 NGM 62 NAM 59 NGM 71 NAM 67 NGM 67 NAM 71 NGM[see Annex]

5 - Which of the following statements about stall speed is correct? Use of a T-tail will decrease the stall speed Increasing the angle of sweep of the wing will decrease the stall speed Increasing the anhedral of the wing will decrease the stall speed Decreasing the angle of sweep of the wing will decrease the stall speed

6 - An aircraft may be weighed In an area of the airfield set aside for maintenance. In a quiet parking area clear of the normal manoeuvring area. At a specified 'weighing location' on the airfield. In an enclosed, non-air conditioned, hangar.

7 - The block diagram of an auto-pilot is shown in the annex.For each control channel (pitch, roll and yaw) the piloting law is the relationship between the deflection of the control surface commanded by the computer (BETA c) and the:

Pilot command E. Aircraft response S. Offset EPSILON at the computer input. Real deflection of the control surface (BETA control surface feedback).

8 - If an aircraft is flying (with flaps and landing gear retracted) in proximity to terrain and its GPWS (Ground Proximity Warning System) get activated, because it is detecting that the aeroplane has an excessive rate of descent, the system provides the following aural warning signals: 'SINK RATE, SINK RATE' followed by 'WHOOP WHOOP PULL UP' (twice) 'TOO LOW, TERRAIN' (twice) followed by 'TOO LOW GEAR' (twice) 'TERRAIN, TERRAIN' followed by 'WHOOP WHOOP PULL UP' (twice) 'DON'T SINK, DON'T SINK'

9 - A location in the aircraft which is identified by a number designating its distance from the datum is known as: Station. Index. MA Moment.

10 - Which of the following qualitative statements about a fixed propeller optimized for cruise condition, is true for the take-off case? The angle of attack of the propeller: Blade is relatively high. Blades reduces to zero. Airfoil section is negative. Blade Is Relatively Small.

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