Functional Test of the VOR/MKR
TASK 34-55-00-720-001-A
Functional Test of the VOR/MKR
To make sure that the VOR and MKR systems operate correctly.
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
B. Referenced Information
3. Job Set-up
Subtask 34-55-00-865-053-A
Subtask 34-55-00-720-050-B ** ON A/C NOT FOR ALL
Subtask 34-55-00-860-053-A
[Rev.10 from 2021]
2026.04.01 12:36:18 UTC
Functional Test of the VOR/MKR
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.
NOTE: You can do the MKR test only at the end of the VOR1 test.
1. Reason for the JobTo make sure that the VOR and MKR systems operate correctly.
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | AR | TEST UNIT-GROUND,VOR/MKR |
| 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 34-55-00-865-053-A
A. Make sure that this(these) circuit breaker(s) is(are) closed:
Subtask 34-55-00-860-052-A ** ON A/C NOT FOR ALL | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 49VU | NAV/VOR/DME/RMI | 12FN | F13 |
| ** ON A/C ALL | |||
| 49VU | NAV/VOR/1 | 2RS1 | G13 |
| 121VU | COM NAV/VOR/2 | 2RS2 | K08 |
B. Aircraft Maintenance Configuration
(1) Energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-861-002)
(2) Install the TEST UNIT-GROUND,VOR/MKR near the VOR or MKR antenna as shown in the installation instructions.
(3) Do the ADIRS start procedure (Ref. AMM TASK 34-10-00-860-002).
(4) Do the IR alignment procedure (Ref. AMM TASK 34-10-00-860-004).
(5) On the EFIS control sections of the FCU:
(7) On the center pedestal, on the RMP1 and RMP2:
Subtask 34-55-00-860-052-B ** ON A/C NOT FOR ALL (1) Energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-861-002)
(2) Install the TEST UNIT-GROUND,VOR/MKR near the VOR or MKR antenna as shown in the installation instructions.
(3) Do the ADIRS start procedure (Ref. AMM TASK 34-10-00-860-002).
(4) Do the IR alignment procedure (Ref. AMM TASK 34-10-00-860-004).
(5) On the EFIS control sections of the FCU:
- set the ADF/VOR selector switches to VOR and the mode selector switches to ROSE/VOR.
- push the ILS pushbutton switches.
(7) On the center pedestal, on the RMP1 and RMP2:
- set the ON/OFF selector switch to ON.
B. Aircraft Maintenance Configuration
(1) Energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-861-002)
(2) Install the TEST UNIT-GROUND,VOR/MKR near the VOR or MKR antenna as shown in the installation instructions.
(3) Do the ADIRS start procedure (Ref. AMM TASK 34-10-00-860-002).
(4) Do the IR alignment procedure (Ref. AMM TASK 34-10-00-860-004).
(5) On the EFIS control sections of the FCU:
(7) On the center pedestal, on the RMP1 and RMP2:
4. Procedure(1) Energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-861-002)
(2) Install the TEST UNIT-GROUND,VOR/MKR near the VOR or MKR antenna as shown in the installation instructions.
(3) Do the ADIRS start procedure (Ref. AMM TASK 34-10-00-860-002).
(4) Do the IR alignment procedure (Ref. AMM TASK 34-10-00-860-004).
(5) On the EFIS control sections of the FCU:
- set the ADF/VOR selector switches to VOR and the mode selector switches to ROSE/VOR.
- push the ILS pushbutton switches.
(7) On the center pedestal, on the RMP1 and RMP2:
- set the ON/OFF selector switch to ON.
- set the VOR/ADF selector switches to VOR.
Subtask 34-55-00-720-050-B ** ON A/C NOT FOR ALL
A. Test of the VOR Reception and Identification
Subtask 34-55-00-720-050-D ** ON A/C NOT FOR ALL | ACTION | RESULT |
|---|---|
| 1.On the test unit: | |
| |
| 2.On the RMP1 (RMP2): | |
| On the RMP, the green LED on this pushbutton switch comes on. |
| On the RMP, the green LED on this pushbutton switch comes on. |
| On the RMP1 (RMP2):
|
| On the CAPT and F/O NDs the dagger shaped (course pointer) shows 5° and the lateral deviation bar moves to the left and stops on the first dot. |
| On the CAPT and F/O NDs the dagger shaped (course pointer) shows 10° and the lateral deviation bar moves to the left and stops on the second dot. |
| On the CAPT and F/O NDs the dagger shaped (course pointer) shows 355° and the lateral deviation bar moves to the right and stops on the first dot. |
| On the CAPT and F/O NDs the dagger shaped (course pointer) shows 350° and the lateral deviation bar moves to the right and stops on the second dot. |
| 3.On the test unit: | |
| On the CAPT and F/O NDs:
|
| 4.On the RMP1 (RMP2): | |
| On the CAPT and F/O NDs:
|
| On the CAPT and F/O NDs:
|
5.On the test unit:
| On the CAPT ND:
|
| | On the F/O ND:
|
| | On the VOR/ADF/DME RMI:
|
| 6.On the test unit: | |
| In the loudspeaker, you can hear the audio signal. |
| 7.On the ACP: | |
| The adjustment is continuous and no unwanted noise is heard. |
| 8.On the test unit: | |
| You cannot hear the signal. |
| 9.On the RMP1 (RMP2): | |
| On the RMP, the green LED on this pushbutton switch goes off. |
A. Test of the VOR Reception and Identification
Subtask 34-55-00-720-050-E ** ON A/C NOT FOR ALL | ACTION | RESULT |
|---|---|
| 1.On the test unit: | |
| |
| 2.On the RMP1 (RMP2): | |
| On the RMP, the green LED on this pushbutton switch comes on. |
| On the RMP, the green LED on this pushbutton switch comes on. |
| On the RMP1 (RMP2):
|
| On the CAPT and F/O NDs the dagger shaped (course pointer) shows 5° and the lateral deviation bar moves to the left and stops on the first dot. |
| On the CAPT and F/O NDs the dagger shaped (course pointer) shows 10° and the lateral deviation bar moves to the left and stops on the second dot. |
| On the CAPT and F/O NDs the dagger shaped (course pointer) shows 355° and the lateral deviation bar moves to the right and stops on the first dot. |
| On the CAPT and F/O NDs the dagger shaped (course pointer) shows 350° and the lateral deviation bar moves to the right and stops on the second dot. |
| 3.On the test unit: | |
| On the CAPT and F/O NDs:
|
| 4.On the RMP1 (RMP2): | |
| On the CAPT and F/O NDs:
|
| On the CAPT and F/O NDs:
|
5.On the test unit:
| On the CAPT ND:
|
| | On the F/O ND:
|
| | On the VOR/ADF/DME RMI:
|
| 6.On the test unit: | |
| In the loudspeaker, you can hear the audio signal. |
| 7.On the ACP: | |
| The adjustment is continuous and no unwanted noise is heard. |
| 8.On the test unit: | |
| You cannot hear the signal. |
| 9.On the RMP1 (RMP2): | |
| On the RMP, the green LED on this pushbutton switch goes off. |
A. Test of the VOR Reception and Identification
Subtask 34-55-00-720-051-A ** ON A/C NOT FOR ALL | ACTION | RESULT |
|---|---|
| 1.On the test unit: | |
| |
| 2.On the RMP1 (RMP2): | |
| On the RMP, the green LED on this pushbutton switch comes on. |
| On the RMP, the green LED on this pushbutton switch comes on. |
| On the RMP1 (RMP2):
|
| On the CAPT and F/O NDs the dagger shaped (course pointer) shows 5° and the lateral deviation bar moves to the left and stops on the first dot. |
| On the CAPT and F/O NDs the dagger shaped (course pointer) shows 10° and the lateral deviation bar moves to the left and stops on the second dot. |
| On the CAPT and F/O NDs the dagger shaped (course pointer) shows 355° and the lateral deviation bar moves to the right and stops on the first dot. |
| On the CAPT and F/O NDs the dagger shaped (course pointer) shows 350° and the lateral deviation bar moves to the right and stops on the second dot. |
| 3.On the test unit: | |
| On the CAPT and F/O NDs:
|
| 4.On the RMP1 (RMP2): | |
| On the CAPT and F/O NDs:
|
| On the CAPT and F/O NDs:
|
5.On the test unit:
| On the CAPT ND:
|
| | On the F/O ND:
|
| 6.On the test unit: | |
| In the loudspeaker, you can hear the audio signal. |
| 7.On the ACP: | |
| The adjustment is continuous and no unwanted noise is heard. |
| 8.On the test unit: | |
| You cannot hear the signal. |
| 9.On the RMP1 (RMP2): | |
| On the RMP, the green LED on this pushbutton switch goes off. |
B. Test of the MKR Reception and Identification
Subtask 34-55-00-720-051-B ** ON A/C NOT FOR ALL | ACTION | RESULT |
|---|---|
| 1.On the test unit: | |
| On the CAPT and F/O PFDs:
|
| 2.On the ACP: | |
| In the loudspeaker, the adjustment is continuous and no unwanted noise can be heard. |
| 3.On the test unit: | |
| On the CAPT and F/O PFDs:
|
| On the CAPT and F/O PFDs:
|
| On the CAPT and F/O PFDs: the last MKR indication goes out of view. In the loudspeaker, you cannot hear the transmission of the audio signal. |
B. Test of the MKR Reception and Identification
5. Close-up| ACTION | RESULT |
|---|---|
| 1.On the test unit: | |
| On the CAPT and F/O PFDs:
|
| 2.On the ACP: | |
| In the loudspeaker, the adjustment is continuous and no unwanted noise can be heard. |
| 3.On the test unit: | |
| On the CAPT and F/O PFDs:
|
| On the CAPT and F/O PFDs:
|
| On the CAPT and F/O PFDs: the last MKR indication goes out of view. In the loudspeaker, you cannot hear the transmission of the audio signal. |
Subtask 34-55-00-860-053-A
A. Put the aircraft back to its initial configuration.
(1) On the EFIS control sections of the FCU:
(3) On the center pedestal, on the RMP, set the ON/OFF switch to OFF.
(4) On the center pedestal, on the ACP, release the VOR1 (2) or MKR pushbutton switch.
(5) Stop the test unit.
(6) De-energize the aircraft electrical circuits.
(Ref. AMM TASK 24-41-00-862-002)
(7) 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.
- release the ILS pushbutton switches.
(3) On the center pedestal, on the RMP, set the ON/OFF switch to OFF.
(4) On the center pedestal, on the ACP, release the VOR1 (2) or MKR pushbutton switch.
(5) Stop the test unit.
(6) De-energize the aircraft electrical circuits.
(Ref. AMM TASK 24-41-00-862-002)
(7) Make sure that the work area is clean and clear of tools and other items.
VOR-Frequency and Course Selection