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CPL Test Series
Question Bank
Questions for REMOTE INDICATING MAGNETIC COMPASS
Answer the following questions
Test Mode
Training Mode
1. The heading information originating from the gyro-magnetic compass flux valve is sent to
amplifier
erector system
error detector
heading indicator
2. The input signal of the amplifier of the gyro-magnetic compass resetting device originates from the
flux valve
directional gyro unit
error detector
directional gyro erection device
3. A flux valve senses the changes in orientation of the horizontal component of the earth's magnetic field : 1- the flux valve is made of a pair of soft iron bars 2- the primary coils are fed AC voltage 3- the information can be used by a “flux gate” compass or a directional gyro 4- the flux gate valve casing is dependent on the aircraft three inertial axis 5- the accuracy of the value of the magnetic field indication is less than 0.5% The combination of correct statements is
1, 4 and 5
1, 3, 4 and 5
2, 3 and 5
3 and 5
4. A gyro-magnetic compass or magnetic heading reference unit is an assembly which always consists of : 1- a directional gyro 2- a vertical axis gyro 3- an earth's magnetic field detector 4- an azimuth control 5- a synchronising control The combination of correct statements is
1, 3 and 5
2 and 5
1 and 4
2, 3 and 5
5. A slaved directional gyro derives its directional signal from
the flight director
the air data computer
a direct reading magnetic compass
the flux valve
6. Heading information from the gyro-magnetic compass flux gate is transmitted to the
amplifier
erecting system
error detector
heading indicator
7. The gyro-magnetic compass torque motor
causes the heading indicator to precess
is fed by the flux valve
feeds the error detector system
causes the directional gyro unit to precess
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