Avionics Flashcards

1
Q

What is the normal heading source for each DBDI in flight?

A

The on-side IRS (IRS 1 - left, IRS 2 - right)

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2
Q

What is the backup heading source for each DBDI in flight?

A

IRS #3, indicated by a green “AHDG” indication on each DBDI

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3
Q

What is indicated by a “999” indication in the speed window on the flight guidance panel?

A

No valid auto-speed target is available

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4
Q

What is the default power-up heading source for each DBDI?

A

The flux valve (magnetic compass), indicated by an amber “STBY” on each DBDI

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5
Q

What is the normal order of the FMS pre-departure flow?

A
  • NAV IDENT
  • POS INIT
  • FLIGHT PLAN
  • PERF INIT / PERFORMANCE DATA
  • DEPARTURE
  • TAKEOFF INIT / TAKEOFF DATA
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6
Q

From where do the data acquisition units (DAUs) receive information?

A
  • From the engine sensors

- Misc. aircraft systems such as fuel quantity.

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7
Q

When flying a “blue data” approach, what are the proper indications to show that the FMS is in approach mode?

A
  • At 2 miles prior to the FAF / FAWP, the APRCH light must be illuminated on the CDU
  • The missed approach prompt is not required but should be displayed at the 4L position on the CDU flight plan page
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8
Q

On a “blue data” approach, what is indicated by the illumination of the APRCH light on the FMS CDU? (4)

A
  • FMS is the selected navigation source and
  • aircraft position is 2 NM outside the FAF and the MAP on the FMS LSK 4L
  • The FMS is using sensors approved for that type of approach
  • A non-precision approach that is not localizer-based has been selected from the FMS navigation database
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9
Q

How is CDI scaling affected by the FMS in approach mode?

A

The CDI scaling changes from 5 NM to 1.5 NM either side of center.

(note: G-IV limitations require that all FMS approaches must be coupled to at least the flight director as the CDI does not scale to 0.3)

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10
Q

Is it possible to have both the DGRAD and the APRCH lights on the CDU illuminated at the same time?

A

No, the approach light will not be displayed if DGRAD has illuminated

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11
Q

After takeoff, when are the takeoff V-speeds replaced by VREF on the airspeed tape?

A

When accelerating above 200 knots and altitude above 400’ AGL

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12
Q

What conditions might cause the performance computers to delete the takeoff V-speeds after they have been “boxed” for takeoff?

A

Selecting DIRECT TO a waypoint on the ground

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13
Q

What is the sensor priority for the FMS, from highest to lowest?

A

GPS
DME / DME
VOR / DME
IRS

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14
Q

During an auto-throttle takeoff, when does the auto-throttle system go to “HOLD” mode?

A

At 60 knots indicated airspeed, regardless or power lever position or EPR setting

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15
Q

When are flight director command bars displayed on both PFDs? (3)

A
  • TO or GA mode active
  • Dual approach mode active (ILS below 1,200 feet AGL, both sides have ILS selected an tuned in respective radios)
  • 2 failed symbol generators with the remaining one in NORM (two failed in ALT)
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16
Q

What action is required with a flight guidance computer (FGC) failure?

A

None, the other FGC takes over automatically; FGP selections remain as previously selected

17
Q

What is the indication with a failed fault warning computer (FWC)?

A

A red “X” in the CAS message portion of DU 4 until the operative FWC is selected on the display controller SENSOR page

18
Q

What is the indication with a failed digital air data computer (DADC)?

A

A red “X” on the airspeed, altitude, vertical speed and AOA indications on the affected side until the operative DADC is selected on the display controller SENSOR page

Note: After selection of the operative DADC, the Pressurization panel and Transponder should be checked to ensure an operative DADC is being used.

19
Q

If a data acquisition unit (DAU) channel fails, how can the problem be rectified?

A

Select the operative channel of the affected DAU on the display controller SENSOR page

20
Q

If the captain’s display controller becomes inoperative, what is the effect on the captain’s PFD and ND?

A

All indications will revert to the default power-up display controller values

21
Q

When completing the FMS pre-departure flow, what are the required entries in PERF INIT before PERF DATA can be selected?

A

Cargo weight, number of pax and average pax weight on PERF INIT page 5/5

22
Q

When completing the FMS pre-departure flow, what is indicated by “DEST FUEL REMAINING” on PERF DATA page 2/4?

A

The predicted fuel remaining at the destination, in thousands of pounds

23
Q

What are the different configuration modes of the FMS? (4)

A
  • DUAL - (FMSs share Active FltPlan, Perf, Pilot wpts, stored fltplans, offside radio tuning commands, temp comp config changes, TO / LDG fuel allowance data, custom DB mods, CDU config data, RNP value entries, Uplinked DL info, changes to bank factor)
  • INITIATED TRANSFER (FMSs share pilot wpts, stored fltplans, offside radio tuning commands, temp comp config changes, TO / LDG fuel allowance data, custom DB mods, CDU config data, RNP value entries) FMSs can transfer on command (on last Active FLT PLAN page): Active Flt Plan, Active Flt Plan Edits, Perf Entries
  • INDEPENDENT - (only offside radio tuning commands are transferred to the offside FMS automatically.)
  • SINGLE - No data is transferred between FMSs.
24
Q

What systems and indications might be affected by a DADC failure? (6)

A
  • Airspeed
  • Altimeter
  • Vertical speed
  • AOA
  • Pressurization
  • Transponder
25
Q

What can be expected if an “unflagged” DADC failure (miscompare) occurs in flight?

A

The faulty DADC can be identified by reference to the standby flight instruments

26
Q

On takeoff, when do the autothrottles set the power to the climb EPR target (CLB)?

A

Above 400 feet AGL with FLCH, VS or VNAV selected

27
Q

What CAS message indicates a loss of the active lateral mode of navigation?

A

An amber or blue CPL DATA INVALID CAS message

28
Q

What is the length of time that the cockpit voice recorder (CVR) records voice signals transmitted by the crew members?

A

30 minutes