04/09/21
Message Overview:
Message Description:
Right engine anti-ice control valve fault 7.
[MCID 1208]
Anti-Ice Control Valve 7.
Detection of a fault within the harness between the engine anti-ice control valve and the ECU A/B.
Possible Causes:
- Harness from Inline Splice Connector to +28 VDC Source
- Wiring Harness (W3)
- Wiring Harness (W6)
- Wiring Harness (W1)
- Anti-ice Valve
- Aircraft 28 Volt Power
Troubleshooting Tips:
Advisory Wire/Service Bulletin: None
Forum Articles/Infoservice/Newsletter: None
Quick Links:
| Removal of the Anti-Ice Dual Pressure Switch | AMM 30-21-03-000-801 |
| Installation of the Anti-Ice Dual Pressure Switch | AMM 30-21-03-400-801 |
| Removal of the Engine Electronic Control Unit (ECU) | AMM 76-10-05-000-801 |
| Installation of the Engine Electronic Control Unit (ECU) | AMM 76-10-05-400-801 |
| Wiring - Maintenance Practices - ALL | SPM 20-12-00-02 |
| Wire Repair - Maintenance Practices - ALL | SPM 20-12-10-02 |
Troubleshooting Recommendations:
- MCID 1208 fault present, troubleshoot using the following steps for aircraft and engine fault isolation with reference to the Light Engine Maintenance Manual Subtask 72-00-00-810-203-A01.