11 Navigation Systems Flashcards

1
Q

a. Which systems supplies position information to the FMCs?

b. What happens in the event of an IRS failure?

A

a. Left and right GPS receivers are independent and supply very accurate position data to the IRS. The IRS in turn supplies a very accurate hybrid GPS-inertial position to the FMC.
b. The GPS supplies position and track data directly to the FMC

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2
Q

How many pitot/static systems supply air data to the Air Data Reference System (ADRS)?

A

Three, left, center and right.

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3
Q

If voted ADRS air data is invalid and the AIR DATA/ATT switch is in AUTO, which systems supply backup airspeed and /or altitude?

A

Backup airspeed (AOA SPD) and/or backup altitude (GPS ALT) are automatically provided by the IRS and GPS systems.

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4
Q

What is the source of altitude and airspeed if both voted and backup air data is unavailable?

A

Integrated Standby Flight Display (ISFD) altitude and airspeed are displayed on the PFDs

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5
Q

What are the major components of the Inertial Reference System (IRS)?

A

The inertial reference units (IRUs), and attitude and heading reference units (AHRUs)

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6
Q

How do the IRUs compute position information?

A

The IRUs combine inertial reference functions with GPS position information to provide hybrid GPS-inertial position output

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7
Q

a. What power is required for initial IRS alignment?

b. Are attitude and heading/track shown on the PFD during alignment?

A

a. Battery bus power. b. No.

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8
Q

On the ground, if electrical power is removed, and the battery switched off, leaving the IRS switches ON; what happens?

A

The hot battery bus continues to supply power to the IRS, the ON BAT light illuminates and the ground crew call horn sounds.

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9
Q

When must the crew enter the aircraft position on the CDU POS INIT page?

A

If the GPS position is not available during the alignment.

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10
Q

What do the following CDU help window messages indicate?

a. INERTIAL/ORIGIN DISAGREE
b. ENTER INERTIAL POSITION
c. ALIGNMENT REINITIATED

A

a. The latitude/longitude position is not close to the position of the origin airport.
b. The crew–entered latitude/longitude position does not pass internal IRU comparison tests.
c. The new airplane present position entry fails the internal check twice. The system automatically starts a new alignment cycle

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11
Q

a. What, if anything, can be done after a power interrupt causes an in-flight loss of alignment of an IRU?
b. When is this capability not available?

A

a. The IRU can complete an alignment whilst in flight.

b. When the GPS receivers are not functioning

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12
Q

How long can the IRU remain in NAV mode before a position update?

A

A position update is recommended if the total time in the navigation mode is expected to exceed 18 hours

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13
Q

In the event of both IRUs failing, which systems supply position information to the FMC?

A

A hybrid GPS-inertial position solution using the AHRUs inertial sensors combined with GPS position.

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14
Q

a. What has happened if the EICAS caution message NAV INERTIAL SYS
displays?
b. Are the LNAV/VNAV AFDS modes still available?
c. Are the ND map modes still available?

A

a. Both AHRUs and both IRUs have failed.
b. No.
c. Yes.

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15
Q

If the NAV INERTIAL SYS message is displayed, which systems provide the following data: -
(Refer to the FCOM IRS Schematic ‘With NAV INERTIAL SYS Message’)
a. Altitude/airspeed?
b. Attitude?
c. Heading?
d. Positionandtrackdata?

A

a. ADRS.
b. ISFD.
c. Heading must be manually set on the CDU POS INIT page.
d. GPS

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16
Q

How many ADF systems are fitted?

A

Two.

17
Q

Are the ADF systems tuned manually or automatically?

A

Manually tuned from the left or right CDU on the NAV RADIO page.

18
Q

Where are the left and right ADF bearings automatically displayed?

A

PFD mini-maps.

19
Q

What manual entry must be made to tune an ADF for BFO reception?

A

The frequency and suffix letter “B”.

20
Q

How many ILS receivers are installed?

A

Two.

21
Q

How is the ILS frequency and front course selected?

A

They are usually tuned by the FMC, but can be tuned manually on the NAV RADIO page.

22
Q

What two conditions must be met for FMC ILS autotuning to occur?

A
  1. An ILS, LOC, back course, LDA or SDF approach selected to the active route.
  2. The airplane is within 50 NM from the top of descent, 150 NM of the landing runway threshold, or the FMC is in descent mode.
23
Q

ILS autotuning is inhibited for 10 minutes after initial takeoff. What must be done if an immediate return to the origin airport is required?

A

Selection and execution of a new approach in the active flight plan causes the ILS to autotune to the new approach frequency, even if this is accomplished during the 10 minute takeoff inhibit period.

24
Q

How can the ILS be tuned if all three FMC’s have failed?

A

The left ILS can be tuned from ALTN NAV RADIO page 2/2 on the TCP

25
Q

What does the word PARK adjacent to the ILS - GLS line on the NAV RADIO page mean?

A

The ILS or GLS is not being used and is not tuned.

26
Q

How many VOR/DME systems are installed?

A

Two.

27
Q

Can the VOR/DME systems be automatically tuned by the FMC?

A

Yes.

28
Q

What tuning methods are indicated by the white letters P; R; A and M on the NAV RAD page adjacent to the tuned VORs?

A
  • P (procedure autotuning)–FMC selects nav aids for approach or departure procedure guidance.
  • R (route autotuning)–FMC selects nav aids on the active route.
  • A (autotuning)–FMC selects a nav aid for best position orientation.
  • M (manual)–VOR is manually tuned
29
Q

Is the current radial for a tuned VOR/DME displayed on the NAV RAD page?

A

Yes.

30
Q

How are the two transponders controlled?

A

Through the TCP and ATP.

31
Q

a. What specified transponder/TCAS control is available with the ATP?
b. What happens if the ATP fails?

A

a. The ATP controls the Transponder/TCAS modes.

b. The Transponder/TCAS modes can be set through the backup function of the TCP.

32
Q

a. Selecting the XPDR mode select key accesses the transponder control pages on the TCP. What transponder controls are available?
b. What do the Captain’s and First Officer’s TCP’s share control of?

A
a.
• Altitude Mode (Absolute or Relative).
• ATC IDENT function.
• Mode A numeric code.
• TCAS envelope (Above, Normal ,or Below).
• Transponder select (Left or Right).
b. 
• IDENT function
• left or right side selection
• XPDR code
33
Q

What happens if the on-side transponder fails?

A

The TCP automatically switches to the cross-side transponder.

34
Q

How is the weather radar controlled?

A

Through the TCP.

35
Q

a. Which controls are used to activate the radar and display returns on an ND and/or mini-map?
b. What must be selected on first to allow these controls to work?

A

a. The WXR switch on the EFIS control panel and the WXR check box on the ND drop-down menu.
b. At least one weather radar system must be selected ON from the TCP SYS POWER screen.

36
Q

What is the maximum range that weather returns can be seen on the ND?

A

320 NM.

37
Q

What is the maximum range at which turbulence returns are processed?

A

40 NM.

38
Q

What colour is used to display turbulence?

A

Magenta