07/02/21
Message Overview:
Message Name:
RIGHT HIGH-PRESSURE-BLEED SHUT-OFF VALVE MECHANICALLY FAILED CLOSED
| Message Code: | 361OBS013 |
| Effectivity: | All |
| System: | Bleed Air System |
| System Description: | 36-11-00 |
| Schematic Diagram: | 36-11-00 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Wiring Diagram: | 30-11-01 [ Global Express ] [ G5000 ] [ Global XRS ] 36-11-01 [ Global Express ] [ G5000 ] [ Global XRS ] |
Message Description:
The Right High-Pressure-Bleed Shutoff Valve mechanically failed closed.
Possible Causes:
- High-Pressure-Bleed Shutoff Valve
- Secondary Power Distribution Assembly (SPDA) 3 (A15)
- Associated Wiring
Troubleshooting Tips:
Advisory Wire/Service Bulletin: None
Forum Articles/Infoservice/Newsletter: None
Quick Links:
| 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 Secondary-Power Distribution Assemblies | AMM 24-62-01-000-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Installation of the Secondary-Power Distribution Assemblies | AMM 24-62-01-400-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Removal of the High-Pressure-Bleed Shutoff Valve | AMM 36-11-01-000-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Installation of the High-Pressure-Bleed Shutoff Valve | AMM 36-11-01-400-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Operational Test of the High-Pressure-Bleed Shutoff Valve | AMM 36-11-01-710-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Access to System Diagnostics | AMM 45-45-00-970-804 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Removal of the External Avionics-Compartment Access-Panel (140BB) |
AMM 52-45-11-000-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Installation of the External Avionics-Compartment Access-Panel (140BB) |
AMM 52-45-11-400-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Start the Engine | AMM 71-00-00-866-806 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Engine Shutdown (Usual) | AMM 71-00-00-866-809 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Opening of the Cowls | AMM 71-10-00-010-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Closing of the Cowls | AMM 71-10-00-410-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Safety Precautions - Maintenance Practices - ALL | SPM 20-00-01-02 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Wire Repair - Maintenance Practices - ALL | SPM 20-12-10-02 [ Global Express ] [ G5000 ] [ Global XRS ] |
Troubleshooting Recommendations:
- On the BLEED−AIR control panel, for the left HPV set the switches that follow:
Switch Position L ENG BLEED AUTO R ENG BLEED OFF XBLEED OFF PACK CONTROL NORM R PACK OFF ANTI−ICE WING OFF - Perform the following:
- Start the left engine
- Set the R ENG THROTTLE until the RH INTERMEDIATE PRESSURE is at 20 PSIG on the screen display PNEUMATIC SYSTEM, BLEED INPUTS
- Select SYSTEM DIAG mode on the CAIMS MAIN MENU display
- Select PNEUMATIC on the ATA SELECTION display
- Select BLEED MANAGEMENT CONTROLLER 2 on the LRU SELECTION display
- Select the BLEED MANAGEMENT CONTROLLER 2 to the RAW DATA page on the LRU SELECTION display
- Check if the R BLEED FAULT message comes ON on the EICAS.
- If the HPV shows closed in amber on the EICAS BLEED/ANTI-ICE synoptic page, continue with next step.
- If the HPV shows open in amber on the EICAS BLEED/ANTI-ICE synoptic page, go to step 6.
- Disconnect the electrical connector P708 from the HPV. Perfrom the voltage check as follows:
From To Expected Result Result P708-1 P708-2 28 VDC - If the voltage is as specified, go to step 8.
- If the voltage is not as specified, continue with next step.
- Disconnect the electrical connector (A15P3) from the SPDA 3. Perform a continuity check between P708 and A15P3 as follows:
From To Result P708-1 A15P3-K P708-2 Ground - If there is no continuity, repair or replace the defective wiring as required and do close out.
- If there is continuity, continue with the next step.
- Disconnect the electrical connector P708 from the HPV. Perform a continuity check as follows:
From To Result J708-4 J708-5 - If there is continuity, go to step 8.
- If there is no continuity, continue with next step.
- Perform a continuity check between P708 and the aircraft ground as follows:
From To Result P708-5 Ground - If there is continuity, repair defective wiring as required and do close out.
- If there is no continuity, continue with next step.
- Replace the Right high-pressure-bleed shutoff valve.
- Do close out.