Avionics Flashcards

1
Q

Whats is the NORMAL heading source for each DBDI in flight

A

The on side IRS

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2
Q

Whats is the BACKUP heading source for each DBDI in flight

A

IRS #3 (Green “AHDG” indication on each DBDI

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3
Q

What is indicated by a “999” in the speed window of the flight guidance panel

A

No valid auto-speed target is available

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4
Q

What is the normal order of the FMS pre departure flow

A
NAV IDENT
POS INIT
FLT PLAN
PERF INIT
DEP
TAKEOFF INIT
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5
Q

Where do the Data Acquisition Units (DAU) receive information

A

From the engine sensors

Misc aircraft systems such as fuel quantity

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6
Q

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

A

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

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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
  • 2 miles prior to the FAF/FAWP, the “APRCH” light must be illuminated on the CDU
  • The missed approach prompt SHOULD be displayed at the 4L position on the CDU flight plan page
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8
Q

On a “blue data” app, what is indicated by the illumination of the APRCH light on the FMS

A
  • FMS is the selected navigation source and the aircraft position is 2nm outside the FAF and the MAP on the FMS(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
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9
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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10
Q

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

A

When accelerating above 200 knots and above 400 feet AGL

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11
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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12
Q

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

A

GPS
DME / DME
VOR / DME
IRS

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13
Q

During takeoff when does the auto- throttle system go to “HOLD’ mode

A

At 60 knots IAS, regardless of PWR LVL position or EPR

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14
Q

When are Flight Director command bars displayed on both PFDs

A

TO or GA mode
Dual approach mode active (ILS below 1,200AGL
2 failed symbol generators with the remaining one in NORM (two failed in ALT)

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15
Q

What action is required with a flight guidance computer failure

A

NONE, the working FGC takes over automatically

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16
Q

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

A

A RED “X” in the CAS message portion of DU4 until the operative FWC is selected on the display controller SENSOR page