Instruments Flashcards

1
Q

Total pressure source is

A

The pitot tube

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2
Q

The 3 basic pressure insturments are _____ and use what source

A

-Airspeed indicator
( pitot pressure and static)

-Altimeter
Vertical speed indicator
(static only)

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3
Q

Position Error

A

Caused by disruption in the airflow over the pressure system source

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4
Q

Indicated airspeed is a measure of

A

Dynamic pressure

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5
Q

To get TAS from IAS you correct with

A

Density error

Postion error

Compressibility error

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6
Q

As aircraft climb altimeter aneroid capsule will

A

Expand due to the static pressure outside is reducing

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7
Q

QNE is

A

Pressure altitude

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8
Q

Before flying IFR the altimeter should read

A

+30 and - 40 on the correct altitude when the aircraft is on the ground.

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9
Q

Inside the VSI

A

Static pressure flows into the capsule then is leaked into the case

If there is more pressure inside the capsule then out, the VSI will show a descent.

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10
Q

Using alternate static will cause altimeter

A

to be slightly high because the pressure inside the cabin is lower.

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11
Q

If the static source is blocked VSI will

A

A slight under read

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12
Q

Rigidity is a gyro desire to

A

Remain in a fixed alignment in space unless acted upon by an external force.

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13
Q

A rate gyro

A

Has freedom of movement in two planes

Movement in the third is used to measure precession.

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14
Q

An Earth gyro is free to move in

A

3 planes but is controlled by gravity to maintain it’s positon relative to Earth.

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15
Q

A pneumatic gyro

A

Uses a high speed jet of air to spin the gyro.

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16
Q

Advantages of electrically driven gyro

A

-Cleaner and less maintenance

-Spin at a higher and more precise RPM

-increased resistance to toppling

17
Q

Gyro inside TI and TC

A

-Spins away from pilot

-In a right turn, the top of the gyro will tip left.

18
Q

The co-ordination ball on a TI/TC is

A

Independent from any power source.

19
Q

HI/DI uses what kind of gyro

A

Tied Gyro

20
Q

HI/DI has it’s spin axis

A

Vertically |||||||

21
Q

The gyro in the Altitude heading is mounted inside 2 gimbal rings

A

-Inner gimbal allows for pitching

-Outer gimbal allows for rolling

22
Q

The pendulous unit

A

Keeps the gyro axis aligned with the true vertical

23
Q

Acceleration error during takeoff will show

A

Climbing turn to the right

24
Q

An electrically driven Altitude indicator

A

-Uses mercury switches

-Connected to torque motors to maintain true vertical

25
Q

Limits for pneumatically driven AI are

A

-55 degrees pitch

-90 degrees roll

26
Q

Limits for electrically driven AI

A

-85 degree pitch

-No limit in roll

27
Q

Flux valve in a RMI

A

is fixed in azimuth but pendulously suspended in damping fluid to allow it to remain horizontal.

28
Q

DGU stands for

A

Directional gyro unit

29
Q

Slaving rate of DGU to the flux valve is aprox

A

1-2 degrees per minute

30
Q

Aparanet wonder is

A

-prominent at poles

-aprox 11 degrees per hour at nz
15 degrees x sin lat/hour

-compensated using drift nut or latitude rider.

31
Q

Gyro inside TC and TI has its axis

A

lateral

32
Q

Signs that ASI pitot has been frozen

A

airspeed will fluctuate then drop to a very small value

pitot pressure leaks out the drain hole

33
Q

Purpose of a pendulous unit on a Artificial horizon is

A

To keep the gyro spin axis aligned with the true vertical

34
Q

what effect of decrease in temperature while aircraft is flying level at FL 190

A

TAS decrease

EAS increase

35
Q
A