# SDR YENA2024111201469

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: November 6, 2024
- Submitted: November 12, 2024
- Operation: Air carrier
- Aircraft: [N571JB](https://openairdocs.org/aircraft/N571JB), registered now
- Make and model: Airbus A320-232
- Registry model: [Airbus A320-232](https://openairdocs.org/model/airbus-a320-232) (OpenAirDocs)
- Aircraft serial: 02125
- Aircraft time: 78,938 hours, 28,634 cycles
- System (JASC): [5322 · Fuselage Internal Mounting Structure](https://openairdocs.org/jasc/5322)
- Part: Door Frame
- Condition: Cracked
- Location: Fwd Galley Area
- 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/YENA2024111201469

## Discrepancy

DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FR 20 RH SIDE FROM HOLE 3 OF JOOGLE AREA LOCATED AT LEVEL OF DOOR STOP FITTING 7 AT FWD GALLEY AREA. CRACK DEPTH I IS 0.045 INCH; (RESOLVED ON W/O: 1318564 TASKCARD: NR-00028) REF AE WO 2024-275/1. N/R# 2024 - 538554. PERFORMED PERMANENT REPAIR ON HOLE 3 FR 20 RH SIDE JOOGLE AREA LOCATED AT LEVEL OF DOOR STOP FITTING 7 AT FWD GALLEY AREA I.A.W. A320 SRM 53-11-12-300-012 STEP 2.A.(1). FINAL DIAMETER OF HOLE IS 0.277 INCH (SECOND OVZ). THIS REPAIR IS CLASSIFIED CATEGORY B AND MUST BE INSPECTED AT 8900FC (FH NOT RELEVANT) FROM TIME OF REPAIR EMBODIMENT AND SUBSEQUENT INSPECTIONS AT INTERVALS OF 8900FC (FH NOT RELEVANT) I.A.W. A320 SRI 53-11-12-205-008 TABLE 2. ACCOMPLISHED BY AE TECH# 8660318. AE QC INSP# 273. FUR-A320-53-01806 ASSIGNED.

---
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.