10/09/24
Message Overview:
Message Name:
BRAKE CONTROL VALVE OUTBD R/BCU/WRG
Message Code:
3245429HA
| Reporting LRU: | Brake Control Unit (BCU) |
| Associated CAS: | NORM BRAKE FAIL (Warning) BRAKE 50% DEGRADED (Caution) R OUTBD BRAKE FAIL (Caution) BRAKE FAULT (Advisory) |
| System Description: | 32-43-00 - Brake Control System |
| Schematic Diagram: | [ G5000 ] [ Global Express ] [ Global XRS ] SSM 32-43-00-101 - Brake Control System - Electrical Schematic |
| Wiring Diagram: | [ G5000 ] [ Global Express ] [ Global XRS ] WM 32-43-00-3_002 - Sheet 2 - Right Hand Side - [9002] [ G5000 ] [ Global Express ] [ Global XRS ] WM 32-43-02-1_001 - Sheet 1 - Right - ALL |
Message Description:
Right Outboard Brake Control Valve (BCV) has been detected failed by the Brake Control Unit (BCU).
Possible Causes:
- Right Outboard Brake Control Valve (MT56)
- Brake Control Unit (BCU) (A71)
- Associated Wiring
Troubleshooting Tips:
Advisory Wire/Service Bulletin:
- AW700-32-0138 - Loss of Normal Braking Upon Landing
- AW700-32-0244 - Operational Procedures to Prevent Freezing Brakes
- AW700-32-0359 - Brake Control System - Data Gathering to Reduce the Brake Control Unit (BCU) No-Fault-Found (NFF) rate
- AW700-32-0513 - Wheel Speed Transducer - Brake System Nuisance Fault Messages
- SB700-32-016 - MODIFICATION - BRAKE CONTROL SYSTEM - PART NO. CHANGE OF THE BRAKE CONTROL UNIT TO GW415-7125-5
Full Throttle Blog/Forum Articles/Infoservice/Newsletter: None
Flight Operation Notifications Manual (FONM): None
NOTES:
- If you replace a brake system component please fill out this questionnaire.
- Check resistance of BCV coil in accordance with BCV resistance check (extracted from CMM 32-43-67).
Quick Links:
| Grounding of the Aircraft | [ G5000 ] [ Global Express ] [ Global XRS ] AMM10-11-00-867-801 |
| Removal of the Covers and Plugs | [ G5000 ] [ Global Express ] [ Global XRS ] AMM10-12-00-020-801 |
| Installation of the Covers and Plugs | [ G5000 ] [ Global Express ] [ Global XRS ] AMM10-12-00-420-801 |
| Standard Aircraft Configuration for Maintenance | [ G5000 ] [ Global Express ] [ Global XRS ] AMM12-00-00-867-801 |
| Aircraft Walkaround (for Maintenance) | [ G5000 ] [ Global Express ] [ Global XRS ] AMM12-00-00-867-802 |
| Connect Electrical Power to the Aircraft | [ G5000 ] [ Global Express ] [ Global XRS ] AMM24-00-00-861-801 |
| Remove the Electrical Power from the Aircraft | [ G5000 ] [ Global Express ] [ Global XRS ] AMM24-00-00-861-802 |
| Electrical/Electronic Safety Precautions | [ G5000 ] [ Global Express ] [ Global XRS ] AMM24-00-00-910-801 |
| Electrostatic Discharge Safety Precautions | [ G5000 ] [ Global Express ] [ Global XRS ] AMM24-00-00-910-802 |
| Operational Test of the Brake System | [ G5000 ] [ Global Express ] [ Global XRS ] AMM32-43-00-710-801 |
| Removal of the Brake Control Unit | [ G5000 ] [ Global Express ] [ Global XRS ] AMM32-43-01-000-801 |
| Installation of the Brake Control Unit | [ G5000 ] [ Global Express ] [ Global XRS ] AMM32-43-01-400-801 |
| Removal of the Brake Control Valve | [ G5000 ] [ Global Express ] [ Global XRS ] AMM32-43-09-000-801 |
| Installation of the Brake Control Valve | [ G5000 ] [ Global Express ] [ Global XRS ] AMM32-43-09-400-801 |
| Access to Active Faults | [ G5000 ] [ Global Express ] [ Global XRS ] AMM45-45-00-970-802 |
| Access to Stored Faults | [ G5000 ] [ Global Express ] [ Global XRS ] AMM45-45-00-970-803 |
| Access to System Diagnostics | [ G5000 ] [ Global Express ] [ Global XRS ] AMM45-45-00-970-804 |
| Flight Deck Effect to Fault Correlations | [ G5000 ] [ Global Express ] [ Global XRS ] AMM45-45-00-970-821 |
| Wire Repair - Maintenance Practices - ALL | [ G5000 ] [ Global Express ] [ Global XRS ] SPM20-12-10-02 |
Troubleshooting Recommendations:
- Interchange right outboard BCV with left outboard BCV.
- If system checks are good, replace right outboard BCV and do close out.
- If fault remains, continue with next step.
NOTE: Check resistance of BCV coil to confirm BCV circuit.- Connect a multimeter or ohmmeter across pins A and B of the servo valve assembly connector.
- Set the meter to display resistance in the 100 Ω range. Measure the circuit resistance.
- The resistance must be 180 to 195 Ω at 65 to 75°F (18 to 24°C)
NOTE: If the resistance is measured at a temperature outside the given range, divide the measured resistance by the applicable correction factor.
Temperature Correction Factors °F Ambient Temp. (°C) 60 (15.6) 61 (16.1) 62 (16.7) 63 (17.2) 64 (17.8) 65 (18.3) 66 (18.9) 67 (19.4) 68 (20.0) 69 (20.6) 70 (21.1) 71 (21.7) Correction Factor 1.022 1.020 1.018 1.015 1.013 1.011 1.009 1.007 1.004 1.002 1.000 0.998 °F Ambient Temp. (°C) 72 (22.2) 73 (22.8) 74 (23.3) 75 (23.9) 76 (24.4) 77 (25.0) 78 (25.6) 79 (26.1) 80 (26.7) 81 (27.2) 82 (27.8) 83 (28.3) Correction Factor 0.996 0.994 0.991 0.989 0.987 0.985 0.983 0.981 0.979 0.977 0.974 0.973 °F Ambient Temp. (°C) 84 (28.9) 85 (29.4) 86 (30.0) 87 (30.6) 88 (31.1) 89 (31.7) 90 (32.2) 91 (32.8) 92 (33.3) 93 (33.9) 94 (34.4) 95 (35.0) Correction Factor 0.970 0.968 0.966 0.964 0.962 0.960 0.958 0.956 0.954 0.952 0.950 0.948 °F Ambient Temp. (°C) 96 (35.6) 97 (36.1) 98 (36.7) 99 (37.2) 100 (37.8) Correction Factor 0.947 0.945 0.943 0.941 0.939
- Perform wiring checks between right outboard BCV and BCU.
- If wiring checks are not good, repair defective wiring as required and do close out.
- If wiring checks are good, continue with next step.
- Replace BCU.
- Do close out.