System Test of the Air Data Reference (ADR) A320

1.Reason for the Job

Self explanatory

2. Job Set-up Information

A. Fixtures, Tools, Test and Support Equipment

REFERENCEQTYDESIGNATION
No specificARACCESS PLATFORM 1M(3 FT)

B. Work Zones and Access Panels

ZONE/ACCESSZONE DESCRIPTION
210CKPT,FWD COMPT BHD TO FLT COMPT BULKHEAD
822

C. Referenced Information

REFERENCEDESIGNATION
Ref. 24-41-00-861-002-AEnergize the Aircraft Electrical Circuits from the External Power
Ref. 24-41-00-861-002-A01Energize the Aircraft Electrical Circuits from the APU
Ref. 24-41-00-861-002-A02Energize the Aircraft Electrical Circuits from Engine 1(2)
Ref. 24-41-00-862-002-ADe-energize the Aircraft Electrical Circuits Supplied from the External Power
Ref. 24-41-00-862-002-A01De-energize the Aircraft Electrical Circuits Supplied from the APU
Ref. 24-41-00-862-002-A02De-energize the Aircraft Electrical Circuits Supplied from the Engine 1(2)
Ref. 31-32-00-860-010-AProcedure to Get Access to the SYSTEM REPORT/TEST NAV Page
Ref. 34-10-00-860-002-AADIRS Start Procedure
Ref. 34-10-00-860-005-AADIRS Stop Procedure

3. Job Set-up

SUBTASK 34-13-00-860-079-A

A. Aircraft Maintenance Configuration

(1) Energize the aircraft electrical circuits Ref. AMM TASK 24-41-00-861-002.

(2) Do the ADIRS start procedure Ref. AMM TASK 34-10-00-860-002.

(3) On the center pedestal, on the MCDU, get the SYSTEM REPORT/TEST/NAV page Ref. AMM TASK 31-32-00-860-010.

(4) On the overhead panel, on the ADIRS CDU, make sure that the OFF legend of the ADR pushbutton switches is off).

SUBTASK 34-13-00-010-056-A

B. Get Access

(1) Put the ACCESS PLATFORM 1M(3 FT) in position at the access door 822.

(2) Open the access door 822.

(3) On the battery power center 105VU:

— Loosen the two screws and remove the protective cover.

SUBTASK 34-13-00-875-067-A

C. Make sure that this(these) circuit breaker(s) is(are) closed:

PANELDESIGNATIONFINLOCATION
49VUAUTO FLT/FCU/19CA1B05
49VUL/G/LGCIU/SYS1/NORM1GAC09
49VUNAV PROBES/ADIRU3/PWR/SWTG8FPF09
49VUNAV PROBES/ADIRU 1/AND AOA 1/26VAC5FP1F07
49VUNAV PROBES/ADIRU1/115VAC4FP1F06
105VUADIRS/ADIRU1/28VDC6FP1C02
121VUAUTO FLT/FCU/29CA2M21
121VUADIRS/ADIRU/2PWR/SHED10FPN10
121VUADIRS/ADIRU/3PWR/SWTG9FPN09
121VUADIRS/ADIRU/2/26VAC AND AOA5FP2N08
121VUADIRS/ADIRU/3/26VAC AND AOA5FP3N07
121VUADIRS/ADIRU/2/115VAC4FP2N06
121VUADIRS/ADIRU/3/115VAC4FP3N05
121VUADIRS/ADIRU/2/28VDC6FP2N04
121VUADIRS/ADIRU/3/28VDC6FP3N03
121VUHYDRAULIC/LGCIU/SYS22GAQ35
121VUHYDRAULIC/LGCIU/SYS1/GRND SPLY52GAQ34

4. Procedure

SUBTASK 34-13-00-740-051-B

A. System Test of the Air Data Reference (ADR)

NOTE:  

The actions and the results of this procedure occur on the MCDU that you use.

It is not necessary to do an IR alignment procedure before you start the system test of the ADR.

ACTIONRESULT
1.Push the line select key adjacent to the ADR 1 (ADR 2, ADR 3) indication.The ADR 1 (ADR 2, ADR 3) page comes into view.
2.Push the line select key adjacent to the SYSTEM TEST indication.The TEST IN PROGRESS indication comes into view.At the end of the test, the TEST OK indication comes into view.
3.Push the line select key adjacent to the RETURN indication.The test procedure stops.

5. Close-up

SUBTASK 34-13-00-860-080-A

A. Put the aircraft back to its initial configuration.

(1) On the MCDU, push the line select key adjacent to the RETURN indication until the CFDS menu page comes into view.

(2) Do the ADIRS stop procedure Ref. AMM TASK 34-10-00-860-005.

(3) De-energize the aircraft electrical circuits Ref. AMM TASK 24-41-00-862-002.

SUBTASK 34-13-00-410-056-A

B. Close Access

(1) Install the protective cover on the battery power center 105VU.

(2) Tighten the two screws.

(3) Close the access door 822.

(4) Remove the access platform(s).

Read me first

All instructions and limitations given in those documents that relate to the resetting of systems both on the ground and in the air must be respected. No reset should be attempted without a thorough appreciation of the technical ramifications. No more than one computer should be reset at any one time. No reset should be attempted in flight unless specifically permitted by the QRH. Maintenance messages remaining after a reset require engineering investigation.

If you encounter an ECAM warning or caution that is not available on our website, please take a photo and send it to our Telegram.

Likewise, if you detect any discrepancies on the site, you can report them directly in our Telegram.

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