Flight Data, Navigation And Instruments Flashcards

1
Q

From where do the ADC’s get pitot/ static information

A

The​ ​ air ​ data ​ system​ ​ consists ​ of​ ​ three ​ pitot• ​static ​ systems,​ ​ two ​ Air​ ​ Data​ ​ Computers ​(ADC),​ ​ two ​ angle-of-attack ​ vanes, ​ and​ ​ two ​temperature ​ probes.​ ​ Pressure ​ information ​ to ​various ​ instruments ​ and systems is ​provided ​directly​ ​ from​ ​ the​ ​ pitot-static ​ system, ​ or ​ indi• ​rectly​ via the​ air data computer.​

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2
Q

What do the ADC’s feed information to

A

Three ​ independent​ ​ pitot-static ​ systems​ ​ pro• ​vide​ ​ pitot​ ​ and​ ​ static ​ pressure​ ​ to ​ various​ ​instruments and​ systems,​ ​ and​ to the​ air data ​computers.​ ​

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3
Q

What happens when an ADC fails ? What can you do about it

A

In the​ event​ of​ a ​fa​ilu​r​e​,​​ an​ alert​ will​ be​ ​pre​• ​sented​ and​ ​ the offside​ ​ ADC​ ​ can​ ​ be​ ​ selected​ ​with ​ the​ ADC​ ​ source ​ select​ p/b​ ​ at​ the​ ​main​​ ​instrument panel. Selection of the offside​ ​ADC is indicated at​ the​ onside source select​ ​and​ altimeter​ set panels

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4
Q

Where do you set the QNH reference pressure

A

The ​ QNH​ ​ reference ​ pressure ​can ​ be​ ​ set​ ​ at​ ​ the​ ​ altimeter​ ​ set ​ panel.

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5
Q

What feeds the standby altimeter and standby ASI

A
System 3 
Standby ALT (static only)
Pitot static system standby ASI
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6
Q

What does the angle of attack vanes provide information for

A

Two ​ ​ vane-type ​ ​ angle-of-attack​ ​ ​ sensors, ​ ​ 1 ​and​ ​ 2, ​ located​ ​ left ​ and​ ​ right​ ​ of​ ​ the​ ​ forward​ ​fuselage, ​ ​ ​ provide ​ ​ ​ angle-of-attack​ ​ ​ informa-​ ​tion​ ​ to ​ the​ ​ respective ​ air​ ​ data ​ computer​, ​AFCAS,​ ​ and​ ​ stall​ ​ prevention ​ system.

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7
Q

Where does the TAS information to the IRS’s come from

A

ADC

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8
Q

From where can you enter data into the IRS’s

A

IDSU and FMS

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9
Q

If an IRS Fails , what do you see and what can you do.

A

Alert is represented, IRS FAULT, ATT AND HDG FLAGS ON PFD

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10
Q

How and from where can you align the IRS’s

A

Align and Nav

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11
Q

How long does the alignment take

A

10 minutes

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12
Q

Can the aircraft be moved during alignment

A

No

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13
Q

What mode will the IRS’s be in after alignment

A

NAV

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14
Q

How could you realign the IRS

A

Align or Nav

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15
Q

Where can the weather radar be displayed

A

On the ND in map or arc mode

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16
Q

Can the pilot display be individually controlled

17
Q

What so dashes in the VOR/DME mean

A

VOR/DME tuned Automatically

18
Q

What can you do if an ILS fails

A

In the event of a failure an alert will be presented and the offside ​ILS can be selected with the ILS source select p/b​ at the main instrument panel

In​ the event of​ a failure an alert​ will be presented and ILS 3 can ​be selected with the ILS source select p/b at the main instrument​ panel

19
Q

When is ILS frequency tuning inhibited

A

Frequency​ tuning​ is ​inhibited​ when​ the​ LAND mode​ is engaged.

20
Q

What can you do when an RA fails

A

In the event​ of​ a failure,​ an alert​ will be presented​ and the offside​ radio altimeter, or​ system 3​ ​radio altimeter​ where fitted,​ can​ be selected with the RA Source Select​ P/B​ at​ the​ main​ ​instrument panel

21
Q

What do the EFIS displays consist of

22
Q

How many EFIS Control panels are there

23
Q

What can you do in case of display unit failure

A

A PFD/ND transfer push button is provided in case of unit failure

24
Q

Where are pitch, roll and heading compared

A

On the PFD, FWC

25
Where is the attitude normally displayed
On each PFD and standby AH
26
Where is ILS information displayed
PFD as well as ND
27
Where is heading and course normally displayed
ND
28
What can be displayed on the RMI
VOR AND DME OR ADF AND DME
29
When is the standby horizon powered
When battery is on or when either eng is running
30
How is avionics cooling accomplished
Avionics compartment, main instrument panel, glare shield, and pedestal are cooled by the ​avionics cooling system.​ ​ The system consists of three blower fans, two suction​ fans, and an ​emergency cooling fan. ​ Cabin air is ducted to the system by the blower fans. ​ The spent air is ​drawn from the system by the suction fans​ and is dumped in the area aft of the forward cargo ​compartment.