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Home > Training for exam quizzes ATPL, PPL(A), PPL(H), BPL Hot Air, BPL Gas, SPL - Sailplane, EASA Drone > Aircraft General Knowledge - Instrumentation - ATPL - Airline Transport Pilot license

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

Test 10 Questions ATPL - Airline Transport Pilot license - Aircraft General Knowledge - Instrumentation, no time limit

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1 - VNE is the maximum speed: Which must never be exceeded With flaps extended in landing position At which the flight controls can be fully deflected Not to be exceeded except in still air and with caution

2 - The spin axis of the turn indicator gyroscope is parallel to the: Pitch axis. Yaw axis. Roll axis. Longitudinal axis.

3 - The operating principle of the vertical speed indicator (VSI) is based on the measurement of the rate of change of: Dynamic pressure Static pressure Kinetic pressure Total pressure

4 - 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'

5 - The position of a Flight Director command bars: Repeats the ADI and HSI information Enables the measurement of deviation from a given position. Indicates the manoeuvres to execute, to achieve or maintain a flight situation. Only displays information relating to radio-electric deviation.

6 - The elements which take part in the local vertical alignment of an inertial strap-down unit are: The accelerometers and gyroscopes. The flow inductors. The accelerometers. The gyroscopes.

7 - On a modern aircraft, the flight director modes are displayed on the: Upper strip of the ND (Navigation Display). Upper strip of the ECAM (Electronic Centralized A/C Management). Upper strip of the PFD (Primary Flight Display). Control panel of the flight director only.

8 - In an inertial navigation system (INS), should the platform be displaced from the horizontal, it would oscillate with a period, called Schuler period, of about: 84 seconds. 64 seconds. 24 minutes. 84 minutes.

9 - 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

10 - An air data computer1. supplies the ground speed and the drift (angle)2. determines the total temperature and the true altitude3. receives the static pressure and the total pressure4. supplies the true airspeed to the inertial unit5. determines the Mach number, the outside (static) air temperature The combination regrouping all the correct statements is: 1 and 2 3, 4 and 5 2, 3 and 4 2 and 5

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