INSTRUMENT SYSTEMS 11.5.1 Flashcards

1
Q

Which flight deck indications occur if the pitot tubes are completely blocked?

A

The airspeed indicators react like altimeters

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2
Q

Which parameter has the greatest effect on the Static Source Error (SSE)?

A

Mach number

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3
Q

Concerning pitot/static systems, what happens if there is an ingress of water and the traps are already full?

A

In the digital ADC, the same transducer type is used for static and pitot pressure

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4
Q

An aircraft is on the ground and the altimeter is set to QNH pressure. What height is displayed?

A

Airport elevation

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5
Q

Which statement is correct about ADIRU?

A

The ADIRU has no pressure transducers, but the computational part of a DADC and IRU are integrated

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6
Q

Why does a vertical gyro require an erection system?

A

To ensure the gyro axis is vertical with reference to the surface of the earth

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7
Q

You fly from Cardiff, which has an actual pressure of 1030hPa, to Edinburgh at indicated altitude of 1000ft. What is your true altitude over Edinburgh when the sea level pressure is 1025hPa?

A

1360ft

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8
Q

Which statement is true concerning ADC data calculations?

A

The analogue ADC calculates all outputs in 3 modules at the same time

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9
Q

What does the slaving annunciation of a compass system indicate?

A

The difference between flux valve heading and the heading indication

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10
Q

Which statement is correct about compass compensation?

A

The deviation is recorded on the ground during a 360° turn

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11
Q

Which components are used to measure the motions along the aircraft axes?

A

Accelerometers

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12
Q

What is the purpose of the stick shaker?

A

To simulate the effect of a real stall in the flight controls

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13
Q

How does the stick shaker move the control column?

A

A motor on the control column causes it to vibrate

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14
Q

What is deviation?

A

It is the angle between magnetic north and compass north

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15
Q

What is the function of the SSEC circuit in an ADC?

A

The SSEC carries out a temperature compensation for the Mach module

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16
Q

Why is there a difference between SAT and TAT indications?

A

During flight, TAT is higher than SAT due to the effect of ram rise

17
Q

The altimeter is set to the standard reference pressure and the actual sea level pressure decreases during flight, what is true?

A

With a constant indicated altitude, the true altitude decreases

18
Q

Which is indicated by pneumatic airspeed indicators?

A

IAS