CHAPTER 34 Flashcards

1
Q

How many different ways can you can tune the VOR?

A

3 - Auto FMGEC, Manual MCDU and Manual on the RMP (On side only Captains RMP VOR 1 & FOs RMP for VOR 2)

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2
Q

What supplies power to the ADMs?

A

The associated ADIRU

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3
Q

What does an ADM do?

A

Converts pressure inputs to ARINC bus digital information for the ADIRU

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4
Q

What is contained In a strapdown Inertial Reference System (IRS)?

A

3 x Accelerometers and 3 x Ring laser gyros

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5
Q

Which ADIRU is fed from the Stby Pitot probe?

A

Number 3

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6
Q

What indication is there that the ADM pneumatic connection is correct?

A

A visible blue ring on the connector indicates correct connection.

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7
Q

Which ADIRUs feed the DDRMI?

A

ADIRU 1 & 3

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8
Q

How long does a normal alignment of the IRS system take?

A

10 Minutes

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9
Q

At what North or South latitude is it not possible to align the IRS system?

A

82 degrees

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10
Q

How do you perform a fast realignment?

A

You can do a fast realignment with the selector switch, which must be turned from NAV to OFF and then back to NAV in less than 5 seconds.
The Inertial Reference (IR) starts a 30-second realignment with existing attitude, heading angles and velocities set to zero.

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11
Q

What indication do you get on the ISIS if your airspeed data is not valid?

A

When the airspeed data is not valid, the airspeed scale is replaced by a red SPD flag.

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12
Q

What systems are contained in the The Multi-Mode Receiver LRU?

A

MMR = ILS + GPS.

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13
Q

Where is the MKR receiver installed?

A

2 identical VOR/MKR receivers are fitted but only 1 MKR system is wired on the aircraft

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14
Q

How do you you tune an ILS Glideslope frequency?

A

By tuning to the paired ILS Localiser frequency

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15
Q

How many satellites make up the aircraft GPS system?

A

The spatial segment is composed of a constellation of 24 satellites.
These satellites are arranged in six separate orbital planes of four satellites each on a circular orbit.

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16
Q

How many satellites does the GPS system require for accurate aircraft position calculation?

A

At least 4

17
Q

What colour is the ILS information displayed on the ND?

A

ILS information is displayed in magenta

18
Q

Normally how is ILS 1 information displayed?

A

The ILS 1 information is displayed on PFD 1 and ND 2

19
Q

What is displayed and where if GPS signal is lost?

A

GPS PRIMARY LOST on the NDs

20
Q

What ?is the purpose of the CFDIU?

A

The Centralized Fault Display Interface Unit (CFDIU) enables tests and trouble shooting to be carried out on the MMR system using the MCDU.

21
Q

When can you use the CFDIU for testing?

A

The test can be done only on ground

22
Q

What principle does RAD ALT operate with?

A

The time between the transmission and the reception of the RA signal is proportional to the A/C height.

23
Q

What is RAD ALTs operating range?

A

RAD ALT operates from 0 ft to 2.500 ft.

24
Q

Where are the RAD ALT LRUs located on the aircraft?

A

AFT Cargo compartment

25
Q

where do TCAS (or T2CAS) indications appear?

A

Both the PFDs and the NDs.

26
Q

What is the purpose of the SUPPRESSOR in the TCAS system?

A

ATC and the Distance Measurement Equipment (DME) operate in the same frequency range. A suppressor signal is transmitted by the operating system to inhibit the other systems and to prevent simultaneous transmission.

27
Q

In the TCAS system where is the barometric altitude transmitted from?

A

The barometric altitude is transmitted via the ATC transponder.

28
Q

How can the TCAS system be tested?

A

The Centralized Fault Display Interface Unit (CFDIU) allows testing and trouble-shooting of the TCAS (or T2CAS if installed) through the MCDU. The tests are only available on ground.

29
Q

Various discrete signals are used for inhibition by equipment with higher priority than the TCAS (or T2CAS). What are these systems?

A

1, Stall
2, WindShear
3, Predictive WindShear (PWS)
4, Enhanced Ground Proximity Warning System (EGPWS) messages.

30
Q

The Distance Measuring Equipment (DME) provides range details of what?

A

The Distance Measuring Equipment (DME) provides a digital readout of the aircraft slant range distance from a selected ground station.

31
Q

What LRU is responsible for flight leg counting in the Navigation systems?

A

Each Landing Gear Control and Interface Unit (LGCIU) sends a discrete signal to the associated DME interrogator. This is ground/flight information used for BITE testing inhibits and to count the flight legs.

32
Q

The ADF is a radio navigation aid, what does it provide?

A

The relative bearing of the aircraft to a selected ground station called Non-Directional Beacon (NDB)

33
Q

How is ADF 1 and ADF 2 displayed on the NDs and optional DDRMI?

A

ADF 1 is represented by a single pointer ADF 2 is represented by a double pointer

34
Q

The VOR system is a radio navigation aid, what does it provide?

A

The VOR system calculates a bearing with respect to magnetic north between the ground station and the aircraft axis. Furthermore, the VOR station provides a Morse identification, which identifies the station.

35
Q

The MKR system is a radio navigation aid used in conjunction with ILS, what does it provide?

A

When the aircraft overflies the MKR, the type of MKR is display on the PFDs in different colours, and is indicated by an aural identification.