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

Test 10 domande ATPL - Airline Transport Pilot license - Aircraft General Knowledge - Instrumentation, tempo libero

1 - During a deceleration phase at constant attitude, the control system of the artificial horizon results in the horizon bar indicating a Nose down attitude. Nose up followed by a nose down attitude. Constant attitude. Nose up attitude.

2 - The QNH is by definition the value of the: Atmospheric pressure at the location for which it is given, corrected for non-standard temperature. Altimeter setting so that the altimeter, on the apron of the aerodrome for which it is given, reads zero. Altimeter setting so that the altimeter, on the apron of the aerodrome for which it is given, reads the elevation. Atmospheric pressure at the level of the ground overflown by the aircraft.

3 - 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

4 - When, in flight, the needle of a needle-and-ball indicator is on the left and the ball on the right, the aircraft is: Turning left with not enough bank Turning right with too much bank Turning right with not enough bank Turning left with too much bank

5 - If the static source of an altimeter becomes blocked during a descent the instrument will: Under-read Gradually indicate zero Indicate a height equivalent to the setting on the millibar subscale Continue to display the reading at which the blockage occurred

6 - The purpose of an airplane automatic trim system is to trim out the hinge moment of the: Elevator(s) Elevator(s), rudder(s) and ailerons. Elevator(s) and rudder(s) Rudder(s)

7 - The range of a low altitude radio altimeter is: 500 ft. 2 500 ft. 10 000 ft. Greater than 10 000 ft.

8 - Concerning the TCAS (Traffic Collision Avoidance System): In one of the system modes, the warning: 'PULL UP' is generated In one of the system modes, the warning: 'TOO LOW TERRAIN' is generated Resolution Advisory (RA) must not be followed without obtaining clearance from ATC No protection is available against aircraft not equipped with a serviceable SSR transponder

9 - Flight Director Information supplied by an FD computer is presented in the form of command bars on the following instrument: RMI Radio Magnetic Indicator. BDHI Bearing Distance Heading Indicator. HSI Horizontal Situation Indicator. ADI Attitude Director Indicator.

10 - In the northern hemisphere, during a take-off run in a westerly direction, a direct reading magnetic compass indicates: An apparent turn to the north. An apparent turn to the south. No apparent turn. An apparent turn to approximately the heading 255°.

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