Interface Test of the IR
TASK 34-14-00-740-001-A
Interface Test of the IR
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
B. Work Zones and Access Panels
C. Referenced Information
3. Job Set-up
Subtask 34-14-00-010-052-A
Subtask 34-14-00-869-072-A ** ON A/C NOT FOR ALL
Subtask 34-14-00-860-051-A
[Rev.10 from 2021]
2026.04.01 04:13:28 UTC
Interface Test of the IR
ZONE: 210
1. Reason for the JobSelf explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | 1 | ACCESS PLATFORM 1M(3 FT) |
| No specific | AR | SAFETY CLIP - CIRCUIT BREAKER |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 210 | CKPT,FWD COMPT BHD TO FLT COMPT BULKHEAD |
| 822 |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 24-41-00-861-002-A | Energize the Aircraft Electrical Circuits from the External Power |
| TASK 24-41-00-861-002-A-01 | Energize the Aircraft Electrical Circuits from the APU |
| TASK 24-41-00-861-002-A-02 | Energize the Aircraft Electrical Circuits from Engine 1(2) |
| TASK 24-41-00-862-002-A | De-energize the Aircraft Electrical Circuits Supplied from the External Power |
| TASK 24-41-00-862-002-A-01 | De-energize the Aircraft Electrical Circuits Supplied from the APU |
| TASK 24-41-00-862-002-A-02 | De-energize the Aircraft Electrical Circuits Supplied from the Engine 1(2) |
| TASK 31-32-00-860-010-A | Procedure to Get Access to the SYSTEM REPORT/TEST NAV Page |
| TASK 31-60-00-860-001-A | EIS Start Procedure |
| TASK 31-60-00-860-002-A | EIS Stop Procedure |
Subtask 34-14-00-010-052-A
A. Get Access
(1) Put the ACCESS PLATFORM 1M(3 FT) in position at access door 822.
(2) Open access door 822.
(3) On battery power center 105VU:
Subtask 34-14-00-860-050-A ** ON A/C NOT FOR ALL (1) Put the ACCESS PLATFORM 1M(3 FT) in position at access door 822.
(2) Open access door 822.
(3) On battery power center 105VU:
- Loosen the two screws and remove the protective cover.
B. Aircraft Maintenance Configuration
(1) Energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-861-002).
(2) Do the EIS start procedure (PFD and ND only) (Ref. AMM TASK 31-60-00-860-001).
(3) On the overhead panel :
(5) On the MCDU, get the SYSTEM REPORT/TEST/NAV page
(Ref. AMM TASK 31-32-00-860-010).
Subtask 34-14-00-860-050-C ** ON A/C NOT FOR ALL (1) Energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-861-002).
(2) Do the EIS start procedure (PFD and ND only) (Ref. AMM TASK 31-60-00-860-001).
(3) On the overhead panel :
- on the FLT CTL panels 23VU and 24VU, release the FAC, ELAC and SEC pushbutton switches. The OFF legends are on.
- on the panel 20VU, on the ADIRS CDU, make sure that the three OFF/NAV/ATT selector switches are at OFF.
(5) On the MCDU, get the SYSTEM REPORT/TEST/NAV page
(Ref. AMM TASK 31-32-00-860-010).
NOTE: This test is for the system 1. For the systems 2 and 3, use the indications between the parentheses.
B. Aircraft Maintenance Configuration
(1) Energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-861-002).
(2) Do the EIS start procedure (PFD and ND only) (Ref. AMM TASK 31-60-00-860-001).
(3) On the overhead panel:
(5) On the MCDU, get the SYSTEM REPORT/TEST/NAV page
(Ref. AMM TASK 31-32-00-860-010).
Subtask 34-14-00-865-058-A (1) Energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-861-002).
(2) Do the EIS start procedure (PFD and ND only) (Ref. AMM TASK 31-60-00-860-001).
(3) On the overhead panel:
- On flight control panels 23VU and 24VU, make sure that the FAC, ELAC and SEC pushbutton switches are released (the OFF legends are on).
- On ADIRS MSU panel 41VU, make sure that the three OFF/NAV/ATT selector switches are set to OFF.
(5) On the MCDU, get the SYSTEM REPORT/TEST/NAV page
(Ref. AMM TASK 31-32-00-860-010).
NOTE: This test is for system 1. For systems 2 and 3, use the indications between the parentheses.
C. Make sure that this(these) circuit breaker(s) is(are) closed:
Subtask 34-14-00-865-059-A | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 49VU | NAV PROBES/ADIRU3/PWR/SWTG | 8FP | F09 |
| ** ON A/C NOT FOR ALL | |||
| 49VU | AUTO FLT/FCU/1 | 9CA1 | B05 |
| ** ON A/C ALL | |||
| 49VU | L/G/LGCIU/SYS1/NORM | 1GA | C09 |
| 49VU | NAV PROBES/ADIRU 1/AND AOA 1/26VAC | 5FP1 | F07 |
| 49VU | NAV PROBES/ADIRU1/115VAC | 4FP1 | F06 |
| ** ON A/C NOT FOR ALL | |||
| 49VU | NAV PROBES/ADIRU3/PWR/SWTG | 8FP | F08 |
| ** ON A/C NOT FOR ALL | |||
| 49VU | AUTO FLT/FCU/1 | 9CA1 | H11 |
| ** ON A/C ALL | |||
| 105VU | ADIRS/ADIRU1/28VDC | 6FP1 | C02 |
| ** ON A/C NOT FOR ALL | |||
| 121VU | ADIRS/ADIRU/2PWR/SHED | 10FP | N10 |
| ** ON A/C ALL | |||
| 121VU | AUTO FLT/FCU/2 | 9CA2 | M21 |
| 121VU | ADIRS/ADIRU/3PWR/SWTG | 9FP | N09 |
| 121VU | ADIRS/ADIRU/2/26VAC AND AOA | 5FP2 | N08 |
| 121VU | ADIRS/ADIRU/3/26VAC AND AOA | 5FP3 | N07 |
| 121VU | ADIRS/ADIRU/2/115VAC | 4FP2 | N06 |
| 121VU | ADIRS/ADIRU/3/115VAC | 4FP3 | N05 |
| 121VU | ADIRS/ADIRU/2/28VDC | 6FP2 | N04 |
| 121VU | ADIRS/ADIRU/3/28VDC | 6FP3 | N03 |
| 121VU | HYDRAULIC/LGCIU/SYS2 | 2GA | Q35 |
| 121VU | HYDRAULIC/LGCIU/SYS1/GRND SPLY | 52GA | Q34 |
| ** ON A/C NOT FOR ALL | |||
| 121VU | ADIRS/2PWR/SHED &/AOA2 MON | 10FP | N10 |
D. Open, safety and tag this(these) circuit breaker(s):
4. Procedure| PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 49VU | AUTO FLT/FAC1/28VDC | 5CC1 | B04 |
| ** ON A/C NOT FOR ALL | |||
| 49VU | AUTO FLT/FAC1/28VDC | 5CC1 | H10 |
| ** ON A/C ALL | |||
| 121VU | AUTO FLT/FAC2/28VDC | 5CC2 | M19 |
Subtask 34-14-00-869-072-A ** ON A/C NOT FOR ALL
A. General
Subtask 34-14-00-740-068-D ** ON A/C NOT FOR ALL NOTE: In the test that follows, we use the name DDRMI for the VOR/DME RMI and the VOR/ADF/DME RMI (refer to the equipment on your aircraft).
B. BITE Test of the IR System
Subtask 34-14-00-740-068-F ** ON A/C NOT FOR ALL | ACTION | RESULT |
|---|---|
| 1.On the ADIRS CDU: | On the ADIRS CDU: |
|
|
| |
| 2.On one MCDU, on the NAV page: | On the MCDU: |
| The IR1 (IR2) (IR3) page comes into view. |
| The IR1 (IR2) (IR3) INTERFACE TEST 1/2 page comes into view. |
| The IR1 (IR2) (IR3) INTERFACE TEST 2/2 page comes into view. |
|
|
| 3.On the ADIRS CDU, set the DATA DISPLAY selector switch to HDG. | On the ADIRS CDU, the left part of the display window shows this true HDG value: 010.0 |
| 4.On the MCDU, push the line key adjacent to the RETURN indication. | The test procedure stops. |
| 5.On the ADIRS CDU: | On the ADIRS CDU: |
| |
|
|
| 6.Do the IR2 test as written in para. 2. | You must get the same results only on the F/O PFD and ND and on the ADIRS CDU (no indication on the DDRMI). |
| 7.On the ADIRS CDU: | On the ADIRS CDU: |
| |
|
|
| 8.On the center pedestal, on the SWITCHING panel 8VU, set the ATT/HDG selector switch to CAPT/3. | |
| 9.Do the IR3 test as written in para. 2. | You must get the same results as for the IR1 on the CAPT PFD and ND, the ADIRS CDU and the DDRMI. |
| 10.On the ADIRS CDU, set the OFF/NAV/ATT selector switch related to the IR3 to OFF. | |
B. BITE Test of the IR System
Subtask 34-14-00-740-068-H ** ON A/C NOT FOR ALL | ACTION | RESULT |
|---|---|
| 1.On ADIRS MSU panel 41VU: | On ADIRS MSU panel 41VU: |
|
|
|
|
| |
| 2.On one MCDU, on the NAV page: | On the MCDU: |
| IR1 (IR2) (IR3) page comes into view. |
| IR1 (IR2) (IR3) INTERFACE TEST 1/2 page comes into view. |
| IR1 (IR2) (IR3) INTERFACE TEST 2/2 page comes into view. |
|
|
| 3.On the MCDU, push the line key adjacent to the RETURN indication. | The test procedure stops. |
| 4.On ADIRS MSU panel 41VU: | On ADIRS MSU panel 41VU: |
| |
|
|
| 5.Do IR2 test as written in para. 2. | You must get the same results only on the F/O PFD and ND and on ADIRS MSU panel 41VU (no indication on the DDRMI). |
| 6.On ADIRS MSU panel 41VU: | On ADIRS MSU panel 41VU: |
| |
|
|
| 7.On the center pedestal, on SWITCHING panel 8VU, set the ATT/HDG selector switch to CAPT/3. | |
| 8.Do IR3 test as written in para. 2. | You must get the same results as for IR1 on the CAPT PFD and ND, on ADIRS MSU panel 41VU and the DDRMI. |
| 9.On ADIRS MSU panel 41VU, set the OFF/NAV/ATT selector switch related to the IR3 to OFF. | |
B. BITE Test of the IR System
Subtask 34-14-00-740-068-K ** ON A/C NOT FOR ALL | ACTION | RESULT |
|---|---|
| 1.On ADIRS MSU panel 41VU: | On ADIRS MSU panel 41VU: |
|
|
|
|
| |
| 2.On one MCDU, on the NAV page: | On the MCDU: |
| IR1 (IR2) (IR3) page comes into view. |
| IR1 (IR2) (IR3) INTERFACE TEST 1/2 page comes into view. |
| IR1 (IR2) (IR3) INTERFACE TEST 2/2 page comes into view. |
|
|
| 3.On the MCDU, push the line key adjacent to the RETURN indication. | The test procedure stops. |
| 4.On ADIRS MSU panel 41VU: | On ADIRS MSU panel 41VU: |
| |
|
|
| 5.Do IR2 test given in Para. 2. | You must get the same results only on the F/O PFD and ND, and on ADIRS MSU panel 41VU. |
| 6.On ADIRS MSU panel 41VU: | On ADIRS MSU panel 41VU: |
| |
|
|
| 7.On the center pedestal, on SWITCHING panel 8VU, set the ATT/HDG selector switch to CAPT/3. | |
| 8.Do IR3 test given in Para. 2. | You must get the same results as for IR1 on the CAPT PFD and ND, and on ADIRS MSU panel 41VU. |
| 9.On ADIRS MSU panel 41VU, set the OFF/NAV/ATT selector switch related to IR3 to OFF. | |
B. BITE Test of the IR System
Subtask 34-14-00-740-068-O ** ON A/C NOT FOR ALL | ACTION | RESULT |
|---|---|
| 1.On ADIRS MSU panel 41VU: | On ADIRS MSU panel 41VU: |
|
|
|
|
| |
| 2.On one MCDU, on the NAV page: | On the MCDU: |
| IR1 (IR2) (IR3) page comes into view. |
| IR1 (IR2) (IR3) INTERFACE TEST 1/2 page comes into view. |
| IR1 (IR2) (IR3) INTERFACE TEST 2/2 page comes into view. |
|
|
| 3.On the MCDU, push the line key adjacent to the RETURN indication. | The test procedure stops. |
| 4.On ADIRS MSU panel 41VU: | On ADIRS MSU panel 41VU: |
| |
|
|
| 5.Do IR2 test as written in para. 2. | You must get the same results only on the F/O PFD and ND and on ADIRS MSU panel 41VU (no indication on the DDRMI). |
| 6.On ADIRS MSU panel 41VU: | On ADIRS MSU panel 41VU: |
| |
|
|
| 7.On the center pedestal, on SWITCHING panel 8VU, set the ATT/HDG selector switch to CAPT/3. | |
| 8.Do IR3 test as written in para. 2. | You must get the same results as for IR1 on the CAPT PFD and ND, on ADIRS MSU panel 41VU and the DDRMI. |
| 9.On ADIRS MSU panel 41VU, set the OFF/NAV/ATT selector switch related to the IR3 to OFF. | |
B. BITE Test of the IR System
5. Close-up| ACTION | RESULT |
|---|---|
| 1.On ADIRS MSU panel 41VU: | On ADIRS MSU panel 41VU: |
|
|
|
|
| |
| 2.On one MCDU, on the NAV page: | On the MCDU: |
| IR1 (IR2) (IR3) page comes into view. |
| IR1 (IR2) (IR3) INTERFACE TEST 1/2 page comes into view. |
| IR1 (IR2) (IR3) INTERFACE TEST 2/2 page comes into view. |
|
NOTE: If all cheks have not been performed when the interface test automatically exits, then IR interface test again as described in (2) and resume the procedure where it was stopped. |
| 3.On the MCDU, push the line key adjacent to the RETURN indication or wait until the test automatically exits. | The test procedure stops. |
| 4.On ADIRS MSU panel 41VU: | On ADIRS MSU panel 41VU: |
| |
|
|
| 5.Do IR2 test as written in para. 2. | You must get the same results only on the F/O PFD and ND and on ADIRS MSU panel 41VU. |
| 6.On ADIRS MSU panel 41VU: | On ADIRS MSU panel 41VU: |
| |
|
|
| 7.On the center pedestal, on SWITCHING panel 8VU, set the ATT/HDG selector switch to CAPT/3. | |
| 8.Do IR3 test as written in para. 2. | You must get the same results as for IR1 on the CAPT PFD and ND, on ADIRS MSU panel 41VU. |
| 9.On ADIRS MSU panel 41VU, set the OFF/NAV/ATT selector switch related to IR3 to OFF. | |
Subtask 34-14-00-860-051-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 EIS stop procedure
(Ref. AMM TASK 31-60-00-860-002)
(3) On the FLT CTL panels 23VU and 24VU, push the FAC, ELAC and SEC pushbutton switches. The related OFF legend goes off.
(4) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
Subtask 34-14-00-865-060-A (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 EIS stop procedure
(Ref. AMM TASK 31-60-00-860-002)
(3) On the FLT CTL panels 23VU and 24VU, push the FAC, ELAC and SEC pushbutton switches. The related OFF legend goes off.
(4) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
Subtask 34-14-00-410-052-A | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 49VU | AUTO FLT/FAC1/28VDC | 5CC1 | B04 |
| ** ON A/C NOT FOR ALL | |||
| 49VU | AUTO FLT/FAC1/28VDC | 5CC1 | H10 |
| ** ON A/C ALL | |||
| 121VU | AUTO FLT/FAC2/28VDC | 5CC2 | M19 |
C. Close Access
(1) Install the protective cover on battery power center 105VU.
(2) Tighten the two screws.
(3) Close access door 822.
(4) Remove the access platform(s).
(1) Install the protective cover on battery power center 105VU.
(2) Tighten the two screws.
(3) Close access door 822.
(4) Remove the access platform(s).