# SDR YENA2025011600063

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: January 15, 2025
- Submitted: January 16, 2025
- Operation: Air carrier
- Aircraft: [N505JB](https://openairdocs.org/aircraft/N505JB), registered now
- Make and model: Airbus A320-232
- Registry model: [Airbus A320-232](https://openairdocs.org/model/airbus-a320-232) (OpenAirDocs)
- Aircraft serial: 01173
- Aircraft time: 87,428 hours, 33,098 cycles
- System (JASC): [5311 · Fuselage Main, Frame](https://openairdocs.org/jasc/5311)
- Part: 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/YENA2025011600063

## Discrepancy

DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 20 RH SIDE HOLE A (CONFIRM INDICATION USING BOROSCOPE) IN PASSENGER CABIN (2 EA); (RESOLVED ON W/O: 1347560 TASKCARD: NR-00032) REF AE WO 2024-413/1. N/R# 2024 - 749159. PERFORMED REPAIR ON HOLE A LOC. FRAME 20RH JOGGLE AREA AT LEVEL STOP FITTING 7 IAW A320 SRM 53-11-12-300-012. THIS REPAIR IS CONSIDERED PSE IAW A320 SRM 51-11-12. THIS REPAIR IS CATEGORY B INSPECTION THRESHOLD FROM TIME OF ADL/REPAIR EMBODIMENT 8,900FC(FH NO RELEVANT)SUBSEQUENT INSPECTION INTERVALS UNTIL 60,000FC (FH NOT RELEVANT ) IS 5,900FC(FH NOT RELEVANT) INSPECTION METHOD FOR LEADER HOLE REFER TO SRM 53-11-12-300-012. FIG 14 INSPECTION METHOD FOR ASSOCIATED HOLE PER SRM 53-11-12-300-012. FIG 13. ACCOMPLISHED BY AE TECH# 8623721. AE QC# 174. FUR-A320-53-01932 ASSIGNED.

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