Operational Test of the ADF
TASK 34-53-00-710-002-A
Operational Test of the ADF
Test of ADF Identification and Reception
2. Job Set-up Information
A. Referenced Information
3. Job Set-up
Subtask 34-53-00-860-051-A ** ON A/C NOT FOR ALL
Subtask 34-53-00-710-056-A ** ON A/C NOT FOR ALL
Subtask 34-53-00-860-052-A ** ON A/C NOT FOR ALL
[Rev.10 from 2021]
2026.04.01 01:02:57 UTC
Operational Test of the ADF
WARNING:
MAKE SURE THAT ALL THE CIRCUITS IN MAINTENANCE ARE ISOLATED BEFORE YOU SUPPLY ELECTRICAL POWER TO THE AIRCRAFT. UNWANTED ELECTRICAL POWER CAN BE DANGEROUS.
1. Reason for the JobTest of ADF Identification and Reception
2. Job Set-up Information
A. Referenced Information
| 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 34-10-00-860-002-A | ADIRS Start Procedure |
| TASK 34-10-00-860-004-A | Inertial Reference (IR) Alignment-Procedure |
| TASK 34-10-00-860-004-A-01 | Automatic Inertial Reference (IR) Alignment-Procedure |
| TASK 34-10-00-860-004-A-02 | Inertial Reference (IR) Alignment-Procedure to do a Check of the Links between each Flight Management and Guidance Computer (FMGC) and the three Air Data/Inertial Reference Units (ADIRUs) |
| TASK 34-10-00-860-005-A | ADIRS Stop Procedure |
Subtask 34-53-00-860-051-A ** ON A/C NOT FOR ALL
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) Do the IR alignment procedure
(Ref. AMM TASK 34-10-00-860-004).
(4) On the EFIS control sections of the FCU:
Subtask 34-53-00-860-051-B ** ON A/C NOT FOR ALL (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) Do the IR alignment procedure
(Ref. AMM TASK 34-10-00-860-004).
(4) On the EFIS control sections of the FCU:
- set the ADF/VOR selector switches to ADF
- set the mode selector switches to ROSE/NAV.
- set the ON/OFF switch to ON.
- push the NAV pushbutton switch (the green LED on this pushbutton switch comes on).
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) Do the IR alignment procedure
(Ref. AMM TASK 34-10-00-860-004).
(4) On the EFIS control sections of the FCU:
Subtask 34-53-00-865-054-A (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) Do the IR alignment procedure
(Ref. AMM TASK 34-10-00-860-004).
(4) On the EFIS control sections of the FCU:
- set the ADF/VOR selector switches to ADF
- set the mode selector switches to ROSE/NAV.
- set the ON/OFF switch to ON
- push the NAV pushbutton switch (the green LED on this pushbutton switch comes on).
- set the VOR/ADF selector switches to ADF.
B. Make sure that this(these) circuit breaker(s) is(are) closed:
4. Procedure| PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 49VU | NAV/ADF/1 | 1RP1 | H14 |
| ** ON A/C NOT FOR ALL | |||
| 49VU | NAV PROBES/ADF/1 | 1RP1 | F09 |
| ** ON A/C NOT FOR ALL | |||
| 121VU | COM NAV/ADF/2 | 1RP2 | K02 |
Subtask 34-53-00-710-056-A ** ON A/C NOT FOR ALL
A. Operational Test of the ADF
Subtask 34-53-00-710-056-E ** ON A/C NOT FOR ALL | ACTION | RESULT |
|---|---|
1.On the center pedestal, on one ACP:
| |
| On the CAPT and F/O NDs:
|
| | In the loudspeakers:
|
| 3.On the RMP1 (RMP2): | |
|
|
| 4.On the RMP1 (RMP2): | |
| On the CAPT and F/O NDs, the ADF1 pointer goes out of view. |
| | In the loudspeakers, no signal is heard. |
A. Operational Test of the ADF
Subtask 34-53-00-710-056-G ** ON A/C NOT FOR ALL | ACTION | RESULT |
|---|---|
1.On the center pedestal, on one ACP:
| |
| On the CAPT and F/O NDs:
|
| | In the loudspeakers:
|
| | On the VOR/ADF/DME RMI:
|
| 3.On the RMP1 (RMP2): | |
| In the loudspeakers, you can hear the identification signal but it is weaker. |
| 4.On the RMP1 (RMP2): | |
| On the CAPT and F/O ND, the ADF1 (ADF2) pointer goes out of view. |
| | In the loudspeakers, no signal is heard. |
| | On the VOR/ADF/DME RMI, the ADF1 (ADF2) pointer is in the 3 o'clock position. |
A. Operational Test of the ADF
Subtask 34-53-00-710-056-I ** ON A/C NOT FOR ALL | ACTION | RESULT |
|---|---|
1.On the center pedestal, on one ACP:
| |
| On the CAPT and F/O NDs:
|
| | On the VOR/ADF/DME RMI:
|
| | In the loudspeakers:
|
| 3.On the RMP1 (RMP2): | |
|
|
| 4.On the RMP1 (RMP2): | |
| On the CAPT and F/O ND, the ADF1 pointer goes out of view. |
| | In the loudspeakers, no signal is heard. |
| | On the VOR/ADF/DME RMI, the ADF pointer stays at the position related to the last correct data and the warning flag comes into view. |
A. Operational Test of the ADF
Subtask 34-53-00-710-056-L ** ON A/C NOT FOR ALL | ACTION | RESULT |
|---|---|
1.On the center pedestal, on one ACP:
| |
| On the CAPT and F/O ND :
|
| | In the loudspeakers:
|
| | On the VOR/ADF/DME RMI :
|
| 3.On the RMP1 (RMP2): | |
| In the loudspeakers, you can hear the identification signal but it is weaker. |
| 4.On the RMP1 (RMP2): | |
| On the CAPT and F/O ND, the ADF1 (ADF2) pointer goes out of view. |
| | In the loudspeakers, no signal is heard. |
| | On the VOR/ADF/DME RMI, the ADF1 (ADF2) pointer stays at the position related to the last correct data and the warning flag comes into view. |
A. Operational Test of the ADF
Subtask 34-53-00-710-056-M ** ON A/C NOT FOR ALL | ACTION | RESULT |
|---|---|
1.On the center pedestal, on one ACP:
| |
| On the CAPT and F/O NDs:
|
| | In the loudspeakers:
|
| 3.On the RMP1 (RMP2): | |
|
|
| 4.On the RMP1 (RMP2): | |
| On the CAPT and F/O NDs, the ADF1 pointer goes out of view. |
| | In the loudspeakers, no signal is heard. |
A. Operational Test of the ADF
5. Close-up| ACTION | RESULT |
|---|---|
1.On the center pedestal, on one ACP:
| |
| On the CAPT and F/O NDs:
|
| | On the VOR/ADF/DME RMI:
|
| | In the loudspeakers:
|
| 3.On the RMP1 (RMP2): | |
|
|
| 4.On the RMP1 (RMP2): | |
| On the CAPT and F/O ND, the ADF1 pointer goes out of view. |
| | In the loudspeakers, no signal is heard. |
| | On the VOR/ADF/DME RMI, the ADF pointer stays at the position related to the last correct data and the warning flag comes into view. |
Subtask 34-53-00-860-052-A ** ON A/C NOT FOR ALL
A. Put the aircraft back to its initial configuration.
(1) On the EFIS control sections of the FCU, set the ADF/VOR selector switches to OFF.
(2) DO the ADIRS stop procedure (Ref. AMM TASK 34-10-00-860-005).
(3) On the center pedestal, on the RMP:
(5) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
(6) Make sure that the work area is clean and clear of tools and other items.
Subtask 34-53-00-860-052-B ** ON A/C NOT FOR ALL (1) On the EFIS control sections of the FCU, set the ADF/VOR selector switches to OFF.
(2) DO the ADIRS stop procedure (Ref. AMM TASK 34-10-00-860-005).
(3) On the center pedestal, on the RMP:
- push the NAV pushbutton switch (the green LED on this pushbutton switch goes off)
- set the ON/OFF switch to OFF.
(5) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
(6) Make sure that the work area is clean and clear of tools and other items.
A. Put the aircraft back to its initial configuration.
(1) On the EFIS control sections of the FCU, set the ADF/VOR selector switches to OFF.
(2) Do the ADIRS stop procedure (Ref. AMM TASK 34-10-00-860-005).
(3) On the center pedestal, on the RMP:
(5) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
(6) Make sure that the work area is clean and clear of tools and other items.
(1) On the EFIS control sections of the FCU, set the ADF/VOR selector switches to OFF.
(2) Do the ADIRS stop procedure (Ref. AMM TASK 34-10-00-860-005).
(3) On the center pedestal, on the RMP:
- push the NAV pushbutton switch (the green LED on this pushbutton switch goes off)
- set the ON/OFF switch to OFF.
(5) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
(6) Make sure that the work area is clean and clear of tools and other items.
ADF-Frequency Selection