11.5.1 - Instrument System Flashcards

(28 cards)

1
Q

In an unpressurised aircraft (cessna), the Alternate static source valve can be taken from the ______

A

cockpit

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2
Q

What does the Auxilliary pitot tube feed ?

A

Auto pilot

yaw dampers

overspeed warning system

flight recorded

flight directors

cabin diff. pressure

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3
Q

__________ converts pitot or static pressure into digital output signal through ________ databus

A

ADM (Air Data Module)

ARINC 429

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4
Q

In an altimeter, the bellows are designed with corrugations that allow ____________________

with a change in altitude

A

the expansion to be linear

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5
Q

What baro setting (QNH,QFE or QNE) are aeronautical charts usually set to?

A

QNH

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6
Q

What is the maximum altitude that a radio altimeter can kick in from?

A

2500 ft

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7
Q

__________ minimises static error

A

servo altimeter

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8
Q

Name the types of errors associated with altimeters (6)

A
  1. Scale Error
  2. Hysteresis
  3. After effect
  4. Friction
  5. Case Leak
  6. Barometric scale error
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9
Q

What is the difference between the VSI and altimeter

A

VSI has a pinhole in it which allows an accurately calibrated leak

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10
Q

An IVSI (Instantaneous Vertical Speed Indicator) has a _______

A

pump

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11
Q

The __________ is used for the power setting of the engines

A

TAT (Total air temperature probe)

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12
Q

Aircraft fly at about _____ Mach

A

0.85

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13
Q

Indications on an airspeed indicator are for the following:

Structural limit

Aerodynamic limit

A

Structural limit - Fixed red line (vmo)

Aerodynamic limit - Red barber pole (mmo)

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14
Q

As temperature decreases

The speed of sound ______

A

decreases

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15
Q

Vertical gyro =

Horizontal gyro =

A

Vertical gyro = attitude gyro = (pitch and roll)

Horizontal gyro = directional gyro ( yaw)

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16
Q

What does the Cage or ‘‘Caging’’ knob of a attitude indicator do?

A

Resets the gyro / attitude position

Levels it

17
Q

_______ motors are used to keep gyros rotating

18
Q

The erection control applies for the first 3 minutes of gyro operation a ___________ to the torquer for fast erection at the start up of the gyro

A

higher voltage

(higher voltage at gyro start up to get spinning)

19
Q

A rate gyro has _____ gimbal (____ axis of freedom)

This is tied to ______ and ______

A

A rate gyro has 1 gimbal (1axis of freedom)

This is tied to yawing and precession

20
Q

An attitude gyro has _____ gimbals ( ____ axis of freedom)

this is tied to ____ and _____

based on rigidity in space

A

An attitude gyro has 2 gimbals ( 2 axis of freedom)

this is tied to pitch and roll

based on rigidity in spa

21
Q

Instead of an electric motor, you can have gyro using a ______ or ________

A

venturi or an EDP (engine driven pump)

22
Q

Explain inclination

A

Inclination is the weighted end of the compass pointer at the equator end (not the pointer end) as it tends to point inwards

23
Q

Explain Variation

A

Variation is the difference between True North and Magnetic North (Isogonic lines)

24
Q

Explain Deviation

A

Deviation is the difference between Magnetic North and Compensated North as it needs to compensate for the error in the compass caused by the electrical systems (EMI)

25
The compass heading is correct if the following 3 parameters are met:
1. The aircraft is horizontal 2. There is no acceleration 3. The reading is corrected with the deviation-chart
26
The flux valve is associated with the _____ gyro It is mounted ......
Directional Gyro It is mounted in a wing tip (away from EMI)
27
Lines from East to West are: Lines from North to South are Irelands co-ords are:
Lines from East to West are: Lattitude Lines from North to South are Longitude Irelands co-ords are: 8W 52N
28
What is meant by saying a gyro must be ''strapped down''?
Has to be perfectly level for Gyros and accelerometers