# SDR UALA2010071502531

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: July 14, 2010
- Submitted: July 16, 2010
- Operation: Air carrier
- Aircraft: [N820UA](https://openairdocs.org/aircraft/N820UA), registered now
- Make and model: Airbus A319-131
- Registry model: [Airbus A319-131](https://openairdocs.org/model/airbus-industrie-a319-131) (OpenAirDocs)
- Aircraft serial: 898
- Aircraft time: 40,502 hours, 15,792 cycles
- Engine: Iae V2522A5
- System (JASC): [5310 · Fuselage Main, Structure](https://openairdocs.org/jasc/5310)
- Part: Door Frame
- Condition: Corroded
- Location: R1 Doorway
- Stage of operation: IN
- How discovered: V
- Nature of condition: O
- Precautionary procedure: K
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/UALA2010071502531

## Discrepancy

AFT R1 DOOR FRAME 20 HAS CORROSION AT FLOOR LEVEL IAW UA-EVA-73955, CAT B REPAIR. AREA BLENDED IAW SRM53-11-12, REO-L01257 AND RAS 705 36370-014-2010. DTA 10-046 CREATED TO TRACK. REINSPECT WITHIN 60 00 CYCLES OR 2.5 YEARS AND EVERY 6000 CYCLES OR 2.5 YEARS THERE A FTER VIA HFEC-NTM51-10-08. CURRTG PTC IS 15792, FIRST REINSPECT DUE AT 21792 CYCLES. NR B7211M BY305679 AND INSPECTED BY LC03. CORROSION WAS ON FWD FACE OF FRAME 20.

---
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.