# SDR CALA2015050693661

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: May 5, 2015
- Submitted: May 6, 2015
- Operation: Air carrier
- Aircraft: [N494UA](https://openairdocs.org/aircraft/N494UA), registered now
- Make and model: Airbus A320-232
- Registry model: [Airbus A320-232](https://openairdocs.org/model/airbus-a320-232) (OpenAirDocs)
- Aircraft serial: 1840
- Aircraft time: 40,520 hours, 17,584 cycles
- Engine: Iae V2527A5
- System (JASC): [5330 · Fuselage Main, Plate/Skin](https://openairdocs.org/jasc/5330)
- Part: Skin
- Condition: Cracked
- Location: Fuselage
- 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/CALA2015050693661

## Discrepancy

FUSELAGE SKIN FRAME 35 & CM10 THE LT AFT LOWER HOLE NR 2 HAS CRACK INDICATION 5:00 POSITION.  REPAIRED NR 2 HOLE & INSTALLED FASTENER LT FRAME 35 IAW ECRA 53-30-04940 & THIS IS TEMP REPAIR.  REPAIR OF CRACKED & ELONGATED FASTENER HOLE FRAME 35 BELOW STRINGER 30 LT HAS BEEN APPROVED AS INTERIM FOR 6 MONTHS IAW RDAS 8 0006388-003-2014 ISSUED NOV 7 2014.  A NEW RDAS THAT PROVIDES INSPECTION THRESHOLD MUST BE REC PRIOR TO MAY 7 2014 IF NEW RDAS IS NOT RECEIVED PRIOR TO MAY 7 2015 THE ACFT IS NOT AIRWORTHY.

---
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.