# SDR WX0A2024081932158

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: July 5, 2024
- Submitted: August 19, 2024
- Operation: Air carrier
- Aircraft: [N220NV](https://openairdocs.org/aircraft/N220NV), registered now
- Make and model: Airbus A320-214
- Registry model: [Airbus A320-214](https://openairdocs.org/model/airbus-a320-214) (OpenAirDocs)
- Aircraft serial: 1262
- Aircraft time: 54,273 hours, 33,860 cycles
- System (JASC): [5311 · Fuselage Main, Frame](https://openairdocs.org/jasc/5311)
- Part: Frame
- Condition: Cracked
- Location: Zone 100
- Stage of operation: IN
- How discovered: E
- Nature of condition: O
- Precautionary procedure: K
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/WX0A2024081932158

## Discrepancy

(AIRCRAFT NOT GROUNDED) (DISCREPANCY DISCOVERED DURING AIRCRAFT HEAVY MX VISIT) NRC 2000-0082: S/M   PASSENGER CABIN, CRACK FOUND AT FR 68 STR 22 RH CRACK FOUND ON WEB HORIZONTAL FLANGE / PASSENGER CABIN FR 68 AT STR 22R/H & STOP FITTING #1 REPAIRED AS PER AIRBUS DOSSIER 81431174 IN COMPLIANCE WITH SRM 53-41-12-300-022 REV. 149. REPAIR CLAISSIFED MAJOR CATEGORY B AS PER RDAF 81431174/004/2024#A ALL REPEAT INSPECTION THRESHOLD FROM 1ST FLIGHT AT 1-EXTERNAL SURFACES OF THE FRAME WEB (FWD FACE) AND REPAIR PART WEB (AFT FACE) EXCEPTING UNDERNEATH THE SEAL PROFILE AND THE BRACKETS AT 71600TFC / FH NOT RELEVANT. INTERVAL: TBD METHOD: TBD.   2- FASTENER HOLES AT FRAME WEB, MACHINED REPAIR PART AND SEAL PROFILE / BRACKETS ATTACHMENTS AT 95000 FC / FH NOT RELEVANT INTERVAL: TBD METHOD TBD. SEE AWS 14 FOR THE CONTINUATION OF THIS CORRECTIVE ACTION. REF AAY ERO R5341E0131 R.OO"

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