Loss of the Radio Altimeter Indication during Approach
TASK 34-42-00-810-842-A
Loss of the Radio Altimeter Indication during Approach
1. Possible Causes
A. Referenced Information
3. Fault Confirmation
Subtask 34-42-00-740-114-A 4. Fault Isolation
Subtask 34-42-00-810-096-A
Subtask 34-42-00-740-115-A
[Rev.8 from Aug 2018]
2026.04.04 04:33:11 UTC
Loss of the Radio Altimeter Indication during Approach
1. Possible Causes
- signs of water and corrosion in the connectors of the antennas
- signs of water and corrosion in the coaxial lines of the antennas
- RA reception and transmission antennas
A. Referenced Information
| REFERENCE | DESIGNATION |
|---|---|
| ESPM 2053230 | |
| AMM 34-42-00-740-002 | BITE Test of the Radio Altimeter |
| AMM 34-42-11-000-001 | Removal of the Radio Altimeter Antenna |
| AMM 34-42-11-400-001 | Installation of the Radio Altimeter Antenna |
| AMM 34-42-11-920-001 | Radio Altimeter Antennas and Coaxial Cables Replacement |
Subtask 34-42-00-740-114-A 4. Fault Isolation
Subtask 34-42-00-810-096-A
A. If the tests are OK:
Subtask 34-42-00-810-113-A 5. Close-up- remove the RA reception antennas (5SA1), (5SA2), and the RA transmission antennas (6SA1), (6SA2) AMM 34-42-11-000-001
- do a check for signs of water and corrosion in the connectors of the antennas
- do a check for signs of water and corrosion in the coaxial lines of the antennas
- repair the coaxial lines if necessary ESPM 2053230.
If the fault continues: - replace the RA reception and transmission antennas related to the defective system(s) AMM 34-42-11-000-001 and AMM 34-42-11-400-001.
Subtask 34-42-00-740-115-A
A. Do the test given in para. 3.
Put the aircraft back to its initial configuration.
After the subsequent flight, make sure that the fault does not continue.
Put the aircraft back to its initial configuration.
After the subsequent flight, make sure that the fault does not continue.