# SDR DALA2026012600552

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: January 25, 2026
- Submitted: January 27, 2026
- Operation: Air carrier
- Aircraft: [N349NB](https://openairdocs.org/aircraft/N349NB), registered now
- Make and model: Airbus A319-114
- Registry model: [Airbus A319-114](https://openairdocs.org/model/airbus-a319-114) (OpenAirDocs)
- Aircraft serial: 1815
- Aircraft time: 61,505 hours, 31,413 cycles
- System (JASC): [5311 · Fuselage Main, Frame](https://openairdocs.org/jasc/5311)
- Part: Frame
- Condition: Cracked
- Location: Zone 200
- 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/DALA2026012600552

## Discrepancy

FWD FUSELAGE CROSSBEAM SPLICING FR16 L/H, HOLES "H2" AND "H3" WITH CRACK INDICATION AT FRAME LAYER. CONTACT LIAISON ENGINNERING FOR REPAIR DISPOSITION. REQUESTING REPAIR DISPOSITION. REPAIR MUST BE ACCOMPLISHED PRIOR TO FURTHER FLIGHT. REFER TO EM 5311-01221, AD 2024-04-04, SB A320-53-1295 CONFIG. 5 REV. 01. INSTRUCTIONS TO LIAISON IN EARTH FOLDER: DELTA AA PROJECTS\53\5311\5311-01221. C/A: LOGPAGE UPDATE: REPLACED FWD FUSELAGE FRAME AT FR16 LH DUE TO AT DOOR STOP # 1 AND #7 LEVEL DOUBLE JOGGLE AREA / FASTENER HOLES OUT OF TOLERANCE AND CROSSBEAM SPLICING LH SIDE HOLE H2 AND H3 WITH CRACK INDICATION I/A/W ER/A # 631351-14AD . REV. ORIGINAL.  MAJOR REPAIR.

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