What was found
RIGHT CONTINUITY FITTING CRACKED 1 INCH FROM CENTER LINE, 1 00% SCREEN HEIGHT. MAJOR REPAIR, REMOVED AND REPLACED LT & RT CONTINUITY AS DIRECTED BY REO L25 980 AND IAW REPAIR DWG'S R53112919 AND R53113426 AND EC/R A 5311-03457.
- Difficulty date
- July 31, 2026
- Submitted
- August 24, 2026
- Operation
- Air carrier
- Aircraft
- N839UA
- Make and model
- Airbus A319131
- Aircraft serial
- 1507
- Aircraft time
- 73,437 hours, 33,068 cycles
- Engine
- Iae V2522A5
- System (JASC)
- 5310 · Fuselage Main, Structure
- Part
- Fitting
- Part number
- D53133228200
- Condition
- Cracked
- Location
- Zone 200
- Stage of operation
- IN
- How discovered
- E
- Nature of condition
- O
- Precautionary procedure
- K
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.