# SDR CALA2019030400348

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: March 3, 2019
- Submitted: March 4, 2019
- Operation: Air carrier
- Aircraft: [N459UA](https://openairdocs.org/aircraft/N459UA), registered now
- Make and model: Airbus A320-232
- Registry model: [Airbus A320-232](https://openairdocs.org/model/airbus-a320-232) (OpenAirDocs)
- Aircraft serial: 1192
- Aircraft time: 60,492 hours, 25,408 cycles
- System (JASC): [5310 · Fuselage Main, Structure](https://openairdocs.org/jasc/5310)
- Part: Door Frame
- Part number: D5311254620051
- 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/CALA2019030400348

## Discrepancy

FUSELAGE FR20, RIGHT, DOOR STOP NR 7 UPPER INBD HOLE HAS A CRACK INDICATION AT 1 O'CLOCK AND 5 O''CLOCK POSITIONS, IN FRAME, AS VIEWED FACING FRAME, AD RELATED TASK, A3NB-53-4-6304, PER LC Q NR 9292316, REPAIRED FRAME 20 DOOR STOP NR 7 HOLE NUMBER 1 IAW EC/RA 5311-0209 0 AND SRM 51-72-11-911-001. ACCOMPLISH INITIAL INSP WHEN AIRCRAF T REACHES 41,808 FC. ACCOMPLISH SUBSEQUENT INSPECTIONS AT INTERVALS NOT TO EXCEED 16,400 FLIGHT CYCLES THEREAFTER.

---
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.