# SDR DALA2026081904724

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: August 13, 2026
- Submitted: August 19, 2026
- Operation: Air carrier
- Aircraft: [N378NW](https://openairdocs.org/aircraft/N378NW), registered now
- Make and model: Airbus A320-211
- Registry model: [Airbus A320-211](https://openairdocs.org/model/airbus-industrie-a320-211) (OpenAirDocs)
- Aircraft serial: 2092
- Aircraft time: 63,792 hours, 32,111 cycles
- System (JASC): [5313 · Fuselage Main, Longeron/Stringer](https://openairdocs.org/jasc/5313)
- Part: Stringer
- Condition: Damaged
- 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/DALA2026081904724

## Discrepancy

CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR STRINGER 5L LOCATED BTW FR 43 - FR 45 IN PASSENGER CABIN.  CONFIRMED DT EVALUATION FCS ON EXISTING REPAIR STR 5L LOC. BTW FR 43 - FR 45 IN PAX CABIN UPPER FUSELAGE, ENGINEERING CONTACTED DUE TO NOT COMPLIED WITH REQUIREMENTS REPAIR FOR MINIMUM OF 4 FASTENERS SPACING BTW OUTER FASTENER ROWS & ADYACENT REPAIR & ANY EXISTING DOUBLER REPAIR IAW SRM 51-70-20 FIGURE 003 SHEET 03. ENGINEERING PROVIDED SRM 53-00 -13-300-001. PERFORMED REPAIR INSTRUCTIONS IAW SRM 53-00 -13-300-001, PARAGRAPH 2.  A RECHECK IS REQUIRED DUE TO REPAIRIS CATEGORY B INSPECTION THRESHOLD FROM TIME OF ADL/REPAIR EMBODIMENT 60000 FC OR 120000 FH IAW SRM 53-00-13-205-001, PARAGRAPH 2.A, TABLE 001.

---
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.