# SDR CALA2026061517104

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: June 12, 2026
- Submitted: June 15, 2026
- Operation: Air carrier
- Aircraft: [N472UA](https://openairdocs.org/aircraft/N472UA), registered now
- Make and model: Airbus A320-232
- Registry model: [Airbus A320-232](https://openairdocs.org/model/airbus-a320-232) (OpenAirDocs)
- Aircraft serial: 1435
- Aircraft time: 75,299 hours, 31,953 cycles
- System (JASC): [5210 · Passenger/Crew Doors](https://openairdocs.org/jasc/5210)
- Part: Door
- Part number: D5211000100000B0
- Condition: Damaged
- Location: L1
- 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/CALA2026061517104

## Discrepancy

LOWER AFT CORNER OF L1 DOOR DAMAGED.REMOVED DAMAGE REF SRM 51-27-11.   PERFORMED DOOR SKIN CUT OUT PER STEP 1 OF AVO 17658. REQUESTING INSPECTION OF TRIMMED EDGE PER STEP 2 OF AVO 17658. ACP DISPOSITION 2 ON AVO 17658 NO CRACKS INDICATED REF NTM PT6 51-10-08. COMPLETED DVI OF INTERNAL STRUCTURE PER STEP 3 OF AVO 17658 WITH NO FURTHER FINDINGS. SUBMITTING COMPLETION OF AVO TO ESC. REMOVED CORNER SEAL IAW STEP 4 OF AVO 17658 REV A , REQUESTING INSP TO PERFORM ROTOTEST INSP OF OPEN HOLESAND DVI CHECK PER STEP 5 REMOVED CORNER SEAL IAW STEP 4 OF AVO 17658 REV A , REQUESTING INSP TO PERFORM ROTOTEST INSP OF OPEN HOLES  AND DVI CHECK PER STEP 5 COMPLIED WITH STEP 5 OF AVO17658 REV A REF NTM 51-10-01-250-801-A-01 (HFEC). NO DEFECTS NOTED, OK TO CONTINUE COMPLIED W STEP 6 OF AVO 17658 REV B .   COMPLIED WITH STEPS 7 -9  , REF AVO 17658 REV B FABRICATED PARTS , DRILLED , DEBURRED , CHAMFER ETC,, EXCLUDING COUNTERSINKING REPAIR DOUBLER AND BACK COUNTERSINKING CHANNEL FOR DOUBLE FLUSH RIVET INSTALLATION.

---
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.
