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

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

1 - If OAT increases when at a constant TAS: Mach number decreases. The difference between surrounding conditions and ISA must be known to deduce the Mach number variation. Mach number remains constant. Mach number increases.

2 - 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.

3 - 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

4 - The rate-of-turn is the: Yaw rate in a turn Aircraft speed in a turn Change-of-heading rate of the aircraft Pitch rate in a turn

5 - The gyromagnetic compass torque motor: Causes the directional gyro unit to precess Is fed by the flux valve Feeds the error detector system Causes the heading indicator to precess

6 - The Mach trim system allows to: Search for the ideal CG location by transferring the fuel into the horizontal stabilizer. Increase the longitudinal static stability of the aircraft by changing the horizontal stabilizer according to the Mach number. Interlock the operation of the stick shaker at the oncoming of the high speed stall. Trim the pitch-up tendency at a high Mach number.

7 - 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.

8 - If an EPR is set at a constant barometric pressure, with an increasing OAT, the thrust Remains constant Decreases. Increases Varies according to the characteristics of the engine

9 - 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

10 - The 'Bourdon tube' is used to measure: Quantity. Temperature. A flow rate. Pressure.

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