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Quiz ATPL - Airline Transport Pilot Licence
Test 10 domande atpl, tempo libero
1 - In accordance with JAR-OPS 1, an airplane whose maximum take-off mass exceeds 5 700 kg or whose maximum approved passenger seating configuration is greater than 9 seats and less than 200 seats must be equipped with a:
Crash axe or a crow-bar in the flight deck.
Crow-bar in the flight deck and a crash axe in the passenger compartment.
Crash axe in the flight deck and a crow-bar in the passenger compartment.
Crash axe and a crow-bar in the passenger compartment.
2 - An aircraft at FL310, M0.83, temperature -30°C, is required to reduce speed in order to cross a reporting point five minutes later than planned.Assuming that a zero wind component remains unchanged, when 360 NM from the reporting point Mach Number should be reduced to:
3 - Given:Distance from departure to destination 95 NM True track 105W/V 060/15TAS 140 kt What is the distance of the PET from the departure point?
4 - What is the speed limit (IAS) in airspace class E?
250 kt VFR and IFR, all levels
250 kt only for VFR up to FL 195
250 kt only for IFR up to FL 100
250 kt for IFR and VFR UP TO FL 100
5 - What does the abbreviation 'MLS' mean:
Mean sea level
Minimum safe level
Minimum sector level
Microwave landing system
6 - What determines the longitudinal stability of an aeroplane ?
The effectiveness of the horizontal stabilizer, rudder and rudder trim tab.
The location of the centre of gravity with respect to the neutral point.
The dihedral, angle of sweepback and the keel effect.
The relationship of thrust and lift to weight and drag.
7 - The high lift device shown in the figure is a:
8 - The spin axis of the turn indicator gyro is aligned along the:
Lateral axis of the aircraft.
Longitudinal axis of flight.
Vertical axis of the aircraft.
Longitudinal axis of the aircraft.
9 - Given:Distance from departure to destination 340 NM True track 320W/V 160/40 TAS 110 ktWhat is the distance of the PET from the departure point?
10 - The tanks of a hydraulic system are pressurized:
In Flight Only.
By bleed air coming from the turbine-engine.
By an auxiliary system.
By The Air Conditioning System.
Invia il test per la correzione
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