# SDR YENA2025061300602

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: June 10, 2025
- Submitted: June 13, 2025
- Operation: Air carrier
- Aircraft: [N760JB](https://openairdocs.org/aircraft/N760JB), registered now
- Make and model: Airbus A320-232
- Registry model: [Airbus A320-232](https://openairdocs.org/model/airbus-a320-232) (OpenAirDocs)
- Aircraft serial: 03659
- Aircraft time: 60,091 hours, 21,856 cycles
- System (JASC): [5310 · Fuselage Main, Structure](https://openairdocs.org/jasc/5310)
- Part: Door 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/YENA2025061300602

## Discrepancy

DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 LH SIDE AT OPEN FASTENER HOLE LOWER INBOARD AT DOOR STOP FITTING 1 POSITION, CRACK DIRECTION IS 6 O'CLOCK, CRACK DEPTH IS 0.085 INCH, AT AFT GALLEY AREA (1 EA);   AEROMAN PERFORMED REPAIR. PER SRM 53-41-12-300-008, 53-41-12-300-010 AND SRI 53-41-12-205-009 REPAIR CATEGORY B INSPECTION THRESHOLD FROM TIME OF ADL/REPAIR EMBODIMENT 24500FH,(FC NOT RELEVANT), SUBSEQUENT INSPECTION AT INTERVALS 10,700 FC ((FH NOT RELEVANT), TABLE 2. INSPECTION METHOD: HFEC AND ROTOTEST IAW A320 SRM 53-41-12-205-009. THIS PART IS CONSIDERABLE PSE IAW A320 51-11-12.

---
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.