# SDR YEN2025F00008

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: September 20, 2025
- Submitted: September 23, 2025
- Operation: Air carrier
- Aircraft: [N621JB](https://openairdocs.org/aircraft/N621JB), registered now
- Make and model: Airbus A320-232
- Registry model: [Airbus A320-232](https://openairdocs.org/model/airbus-a320-232) (OpenAirDocs)
- Aircraft serial: 02491
- Aircraft time: 75,160 hours, 27,064 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/YEN2025F00008

## Discrepancy

DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON LOWER INB HOLE OF FR 68 RH DOOR STOP FITTING Ñ1. CRACK DIRECTION 5 OCLOCK. CRACK D= 0.160 INCH;  PERFORMED PERMANENT REPAIR ON LOC. ON LOWER INB HOLE OF FR 68 RH DOOR STOP FITTING #1 IAW A320 SRM 53-41-12-300-008 FIGURE 003 SHEET 1 AND A320 SRM 53-41-12-300-010. THIS REPAIR IS CATEGORY B. INSPECTION THRESHOLD FROM TIME OF ADL/REPAIR EMBODIMENT 24500 FC. SUBSEQUENT INSPECTION AT INTERVALS 10700 FC (FH NOT RELEVANT) INSPECTION METHOD HFEC (REFER TO NTM CHAPTER 51-10-08) AND ROTOTEST (REFER TO NTM CHAPTER 51-10-01) IAW SRM 53-41-12-205-009 TABLE 2. FUR-A320-53-02620ALL WORK ACCOMPLISHED ON AEROMAN WO 2025195/1 NR542181.

---
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.