# SDR CALA2013123194076

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: December 30, 2013
- Submitted: January 2, 2014
- Operation: Air carrier
- Aircraft: [N493UA](https://openairdocs.org/aircraft/N493UA), registered now
- Make and model: Airbus A320-232
- Registry model: [Airbus A320-232](https://openairdocs.org/model/airbus-a320-232) (OpenAirDocs)
- Aircraft serial: 1821
- Aircraft time: 37,519 hours, 16,398 cycles
- Engine: Iae V2527A5
- System (JASC): [7532 · Compressor Bleed Valve](https://openairdocs.org/jasc/7532)
- Part: Bleed Valve
- Condition: Faulty
- Location: Nr 2 Engine
- Stage of operation: IN
- How discovered: O
- Nature of condition: J
- Precautionary procedure: O
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/CALA2013123194076

## Discrepancy

ENG 2 HP VLV FAULT DISPLAYED ON UPPER ECAM SCREEN.  BLEED VLV SECURED CLOSED IAW MEL.  DURING TROUBLE SHOOTING FOUND CONNECTOR BACK SHELL DAMAGED PCN 565-0756 IAW AWM 7 1-51-03 PG1 RDF-T.  REMOVED BACK SHELL, ALL WIRE INSULATION CHECKED GOOD, INSTALLED NEW BACK SHELL & PLUG IAW AWM 71-51-03PG1.  DEACTIVATED NR 2 HP VLV IAW MEL 3611T, VLV STILL FAULTING.  R & R ENG NR 2 HP BLEED VALVE IAW AMM 36-11-51. OPERATIONS & LEAK CHECKED GOOD.  MEL CLEARED, PLACARD REMOVED.

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.
