06/30/21
Message Overview:
Message Name:
RADIO SYSTEM BUS MEMBERS CANNOT TRANSMIT
| Message Code: | 314OBS003 |
| Effectivity: | All |
| System: | Digital Bus System |
| System Description: | 31-44-00 |
| Schematic Diagram: | 31-44-00 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Wiring Diagram: | 31-44-05 [ Global Express ] [ G5000 ] [ Global XRS ] 31-44-06 [ Global Express ] [ G5000 ] [ Global XRS ] 31-44-07 [ Global Express ] [ G5000 ] [ Global XRS ] |
Message Description:
The Radio Management Units (RMUs) and Aircraft Radio Systems cannot transmit data through the Radio System Bus (RSB).
Possible Causes:
- Very High Frequency (VHF) Communication Unit 1 (A1)
- Very High Frequency (VHF) Communication Unit 2 (A2)
- Very High Frequency (VHF) Communication Unit 3 (A226)
- Very High Frequency (VHF) Navigation Unit 1 (A3)
- Very High Frequency (VHF) Navigation Unit 2 (A4)
- Radio Management Unit (RMU) 1 (A25)
- Radio Management Unit (RMU) 2 (A26)
- Integrated Avionics Computer (IAC) 1 (A11)
- Integrated Avionics Computer (IAC) 2 (A10)
- Integrated Avionics Computer (IAC) 3 (A12)
- Radio System Bus (RSB) Termination Resistor
- Associated Wiring
Troubleshooting Tips:
Advisory Wire/Service Bulletin: None
Forum Articles/Infoservice/Newsletter: None
Quick Links:
| Removal of the VHF Communication Unit | AMM 23-11-01-000-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Installation of the VHF Communication Unit | AMM 23-11-01-400-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Removal of the Radio Management Units (RMU) |
AMM 23-81-01-000-802 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Installation of the Radio Management Units (RMU) |
AMM 23-81-01-400-802 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Connect Electrical Power to the Aircraft | AMM 24-00-00-861-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Remove the Electrical Power from the Aircraft | AMM 24-00-00-861-802 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Electrical/Electronic Safety Precautions | AMM 24-00-00-910-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Removal of the Integrated Avionics Computers (IAC) |
AMM 31-41-01-000-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Installation of the Integrated Avionics Computers (IAC) |
AMM 31-41-01-400-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Operational Test of the Digital Bus System | AMM 31-44-00-710-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Removal of the VHF Navigation Units | AMM 34-51-01-000-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Installation of the VHF Navigation Units | AMM 34-51-01-400-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Wire Repair - Maintenance Practices - ALL | SPM 20-12-10-02 [ Global Express ] [ G5000 ] [ Global XRS ] |
Troubleshooting Recommendations:
- Disconnect RMU 1 connector (A25P1), RMU 2 connector (A26P1), VHF Communication Unit 1 connector (A1P1), VHF Communication Unit 2 (A2P1), VHF Communication Unit 3 connector (A226P1), VHF Navigation Unit 1 connector (A3AP1, A3BP1), VHF Naviagation Unit 2 connector (A4AP1, A4BP1), IAC 1 connector (A11BP1, A11CP1), IAC 2 connector (A10BP1, A10CP1) and IAC 3 connector (A12BP1, A12CP1). Perform a continuity check as follows:
For the Primary RSB:From To Result A25P1-V A1P1-10 A25P1-W A1P1-11 A25P1-V A2P1-10 A25P1-W A2P1-11 A25P1-V A226P1-10 A25P1-W A226P1-11 A25P1-V A3BP1-71 A25P1-W A3BP1-81 A25P1-V A4BP1-71 A25P1-W A4BP1-81 A25P1-V A11BP1-70 A25P1-W A11BP1-71 A25P1-V A10BP1-70 A25P1-W A10BP1-71 A25P1-V A12BP1-70 A25P1-W A12BP1-71 A25P1-V A26P1-V A25P1-W A26P1-W For the left secondary RSB:
From To Result A25P1-M A1P1-74 A25P1-N A1P1-61 A25P1-M A226P1-74 A25P1-N A226P1-61 A25P1-M A3AP1-88 A25P1-N A3AP1-102 A25P1-M A11CP1-36 A25P1-N A11CP1-37 A25P1-M A12CP1-36 A25P1-N A12CP1-37 For the right Primary RSB:
From To Result A26P1-M A2P1-74 A26P1-N A2P1-61 A26P1-M A4AP1-88 A26P1-N A4AP1-102 A26P1-M A10CP1-36 A26P1-N A10CP1-37 - If there is no continuity, repair defective wiring as required and do close out.
- If there is continuity, continue with next step.
- Perform a continuity check as follows:
For the Primary RSB:From To Result A25P1-V Ground A25P1-W Ground For the left secondary RSB:
From To Result A25P1-M Ground A25P1-N Ground For the right Primary RSB:
From To Result A26P1-M Ground A26P1-N Ground - If there is continuity, repair defective wiring as required and do close out.
- If there is no continuity, continue with next step.
- Perform a resistance check on the termination-resistors as follows:
For the Primary RSB (R5 and R6):From To Expected Result Result (Test Connector)J242-x J242-y 50 Ohms For the left Secondary RSB (R9 and R38):
From To Expected Result Result (Test Connector)J241-p J241-q 50 Ohms For the right Secondary RSB (R7 and R8):
From To Expected Result Result (Test Connector)J242-z J242-w 50 Ohms - If the resistance value is not as specified above, replace the defective resistor(s) and do close out.
- If the resistance value is as specified above, continue with next step.
- Install the removed LRUs one by one. Perform a test every time an LRU is connected.
- If the fault comes back after re-installing an LRU, isolate the LRU to confirm the fault and replace as required and do close out.
- If the fault does not come back after re-installing an LRU, continue with next step.
- Perform the operational test of the digital bus system (Refer AMM 31-44-00-710-801).
- If the fault is no longer present, do close out.
- If the fault is still present, continue with next step.
- Replace defective IAC.
- Do close out.