11.5 Instruments/Avionics Systems Flashcards

1
Q

You fly from cardiff which has an actual pressure of 1013hcpa to ending indicated altitude of 10000ft, what is your altitude over ending when sea level pressure is 1025?

A

1360

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2
Q

Which of the following statements is true concerning data calculations?

A

The analogue ADC calculates all outspun 3 modules at the same time.

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3
Q

What does the slaving annunciation of a compass system indicate?

A

Indicates the difference between flux valve heading and the heading indication.

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4
Q

Which statement is true about compass compensation?

A

The deviation is recorded on the ground during a 360 turn

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5
Q

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

A

Rate gyro

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6
Q

What is the purpose of stick shaker?

A

To simulate the effect of a real stall on the flight controls.

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7
Q

GIVEN AN AIRCRAFT WITHOUT A PRESSUISED CABIN, ON WHICH A LEAK HAS OCCURRED IN THE STATIC SYSTEM WHILE THE AIRCRAFT IS IN LEVEL FLIGHT, WHICH INDICATIONS DO YOU GET?

A

ALTIMITER (ALT) SHOWS SLIGHTLY INCREASING VALUES, VERTICAL SPEED INDICATION (VSI) SHOWS CORRECT DATA
AIRSPEED INDICATOR (ASI) SLIGHTLY HIGHER
AIRSPEED INDICATORS SHOW DECREASING VALUES.

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8
Q

CONCERNING PITOT STATIC SYSTEMS, WHAT HAPPENS IF THERE IS AN INCREASE OF WATER AND THE TRAPS ARE ALREADY FULL?

A

INSTRUMENTS FLUCTUATE, VERT SPEED AND ALT NORMAL FUNCTION, AIRSPEED IS ZERO

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9
Q

WHICH OF THE FOLLOWING STATEMENTS ARE TRUE FOR THE PRESSURE TRANSDUCERS USED IN ADC’S?

A

In a digital ADC same tranducer type is used for static and pitot pressure

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10
Q

AN AIRCRAFT IS ON THE GROUND AND THE ALTIMITER IS SET TO QNH PRESSURE, WHAT HEIGH IS DISPLAYED?

A

GROUND SEA LEVEL, IF QFE WOULD = 0

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11
Q

WHICH IS CORRECT ABOUT THE ADIRU?

A

THE ADIRU HAS NO PRESSURE TRANSDUCERS BUT THE COMPUTATIONAL PART OF A DADC AND AN IRU ARE INTERGRATED

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12
Q

WHAT DOES A VERTICAL GYRO REQUIRE AN ERECTION SYSTEM?

A

ENSURE GYRO AXIS IS VERTICAL WITH THE REFERENCE TO SURFACE OF THE EARTH

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13
Q

HOW DOES THE STICK SHAKER MOVE THE CONTROL COLOUM?

A

A MOTOR CAUSES THE CONTROL COLOUM TO VIBRATE

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14
Q

WHAT IS DEVIATION?

A

IT IS THE ANGLE BETWEEN THE 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 TEMPERAURE COMPENSATION FOR THE MACH MODULE.

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16
Q

WHY IS THERE A DIFFERENCE BETWEEN SAT AND TAT INDICATION?

A

DURING FLIGHT THE TAT IS HIGHER THAN THE SAT DUE TO THE EFFECT OF RAM RISE.

17
Q

THE ALTIMITER IS SET TO THE STANDARD REFERENCE PRESSURE AND THE ACTUAL SEA LEVEL PRESSURE DECREASES DURING FLIGHT, WHICH IS TRUE?

A

THE PILOT MUST ADJUST THE BARO SETTING TO THE NEW SEA LEVEL PRESSURE.

18
Q

WHICH IS INDICATED BY PNEUMATIC AIRSPEED INDICATORS?

A

INDICATED AIR SPEED (IAS)

19
Q

Which indications happen if the pitots are blocked?

A

Airspeed indicators show decreasing values.