06/21/21
Message Overview:
Message Name:
AUTOTHROTTLE DOES NOT RETARD ON LANDING
| Message Code: | 223OBS001 |
| Effectivity: | All |
| System: | Autothrottle |
| System Description: | 22-30-00 |
| Schematic Diagram: | 34-44-00 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Wiring Diagram: | 34-44-01 [ Global Express ] [ G5000 ] [ Global XRS ] |
Message Description:
Autothrottle did not retard during the landing phase. There was no change in Thrust power when aircraft altitude reached 50 feet.
Possible Causes:
- Radio Altimeter (RAD ALT) Transceiver 1 (A427)
- Radio Altimeter (RAD ALT) Transceiver 2 (A426)
- RAD ALT 1 Receive (RX) Antenna (E111)
- RAD ALT 1 Transmit (TX) Antenna (E113)
- RAD ALT 2 Receive (RX) Antenna (E110)
- RAD ALT 2 Transmit (TX) Antenna (E112)
- Antenna Coaxial cable
- Associated Wiring
Troubleshooting Tips:
Advisory Wire/Service Bulletin: None
Forum Articles/Infoservice/Newsletter: None
NOTE: An undetected failure with the Radio Altitude system could cause a malfunction of the Autothrottle system.
Quick Links:
| Operational Test of the Autothrottle System | AMM 22-30-00-710-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Operational Test of the Radio Altimeter System | AMM 34-44-00-710-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Removal of the Radio Altimeter Transceivers | AMM 34-44-01-000-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Installation of the Radio Altimeter Transceivers | AMM 34-44-01-400-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Removal of the Radio Altimeter Antennas | AMM 34-44-05-000-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Installation of the Radio Altimeter Antennas | AMM 34-44-05-400-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| General Visual Inspection of the L/HIRF Protection of the Radio Altimeter Antennas Connectors | AMM 34-44-05-210-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Wire Repair - Maintenance Practices - ALL | SPM 20-12-10-02 [ Global Express ] [ G5000 ] [ Global XRS ] |
Troubleshooting Recommendations:
- Gather information. Find out what side the Autothrottle was coupled to when the issue occurred. You may ask the crew that experienced the issue if a red RAD flag was displayed on the PFD at the time of failure. There is also a chance that the altitude call-outs did not take place during descent.
- Perform the operational check of the RAD ALT system.
- Physically inspect the affected RAD ALT transceiver.
- If no defects are found continue with next step.
- If defects are found, rectify/replace as required.
- Remove the affected RAD ALT transceiver. Inspect the connectors for proper installation, damage, moisture and contamination.
- If no defects are found continue with next step.
- If defects are found, rectify/replace as required.
- Swap the affected RAD ALT transceiver with the other RAD ALT transceiver. Is the fault still present?
- If YES, continue with next step.
- If NO, replace defective RAD ALT Transceiver.
- Perform a continuity check of the coaxial cables between the RAD ALT Transceiver and the RX and TX antennas. You may also use a Time Domain Reflectometer (TDR) to detect partial damage or kinks in the coaxial cables that may affect transmission of the radio signals. Cable length is approximately 10 feet.
- If no defects are found continue with next step.
- If defects are found, rectify/replace as required.
- Perform a bonding check of the Antennas.
- If bonding is good, replace the antennas.
- If bonding is not good, rectify as required.
- Do close out.