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Aircraft General Knowledge - Instrumentation - ATPL - Airline Transport Pilot license

Test 10 domande Aircraft General Knowledge - Instrumentation, tempo libero

1 - During deceleration following a landing in an easterly direction, a magnetic compass made for the southern hemisphere indicates: A heading fluctuating about 090°. An apparent turn to the north. No apparent turn. An apparent turn to the south.

2 - One of the errors inherent in a ring laser gyroscope occurs at low input rotation rates tending towards zero when a phenomenon known as 'lock-in' is experienced. What is the name of the technique, effected by means of a piezo-electric motor, that is used Zero drop Cavity rotation Beam lock Dither

3 - The operation of the GPWS (Ground Proximity Warning System) is governed by laws taking the aircraft height into account as well as:1- the descent rate 2- the climb rate3- the aircraft configuration 4- the selected engine rpmThe combination regrouping all the correct statements is: 1,3 2,3 2,4 1,2,4

4 - During a climb, the total pressure probe of the airspeed indicator becomes blocked If the pilot maintains a constant indicated airspeed, the true airspeed: Increases until reaching VMO. Decreases by 1% per 600 FT. Decreases until reaching the stall speed.

5 - The most common sensors interfacing a FMS to compute the aircraft position along the flight plan are:1- MLS2- GPS3- VOR4- IRSThe combination which regroups all of the correct statements is: 1, 2. 1, 2, 4. 2, 3, 4. 1, 4.

6 - Compared with a conventional gyro, a laser gyro: Is influenced by temperature Has a longer life cycle Consumes a lot of power Has a fairly long starting cycle

7 - A thermocouple type thermometer consists of: Two metal conductors of different type connected at two points. A single-wire metal winding. A Wheatstone bridge connected to a voltage indicator. Two metal conductors of the same type connected at two points.

8 - Given:Zp = pressure altitude Zd = density altitudeCAS can be obtained from the following data: EAS and Zp. TAS and Zd. TAS and Zp. EAS and Zd.

9 - The initiation of an automatic go-around can be: In a range of approach airspeeds. At 70 kts ± 5 kts only. With no limit of approach airspeeds. At VY ± 5 kts only.

10 - The Ground Proximity Warning System (GPWS) is a system working according to a height span ranging from: 50 ft to 2 500 ft The ground to 500 ft 30 ft to 5 000 ft The ground to 1 000 ft

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