# SDR FDEA202601210089

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: January 21, 2026
- Submitted: January 27, 2026
- Operation: Air carrier
- Aircraft: [N658FE](https://openairdocs.org/aircraft/N658FE), registered now
- Make and model: Airbus A300 F4-605R
- Registry model: [Airbus A300 F4-605R](https://openairdocs.org/model/airbus-industrie-a300-f4-605r) (OpenAirDocs)
- Aircraft serial: 752
- Aircraft time: 39,616 hours, 22,274 cycles
- System (JASC): [5330 · Fuselage Main, Plate/Skin](https://openairdocs.org/jasc/5330)
- Part: Repair
- Condition: Out Of Limits
- Location: Zone 100
- Component: Skin, Airbus
- Component part number: A5377348722600
- Stage of operation: NR
- How discovered: O
- Nature of condition: O
- Precautionary procedure: O
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/FDEA202601210089

## Discrepancy

EXISTING REPAIR ON FUSELAGE SKIN AT FR22-FR23 STGR51L-STGR53L REQUIRES EVALUATION   FOR CONFORMITY THE EXISTING REPAIR ON FUSELAGE SKIN AT FR22 - FR23 STGR51L-STGR53L NO REPAIR RECORD   FOUND. REMOVED THE EXISTING REPAIR AND RE-REPAIRED THE SKIN IAWSRM 53-10-  12 FIG.208. EO: 6-5100-7-5000 D7 PT1 WAS COMPLETED. TITLE: STRUCTURES - REPAIR CATALOG -   A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707. THE REPAIR IS   CATEGORY "B" & IS CLASSIFIED AS MAJOR PER GMM 6-2-100.THE FIRST INSPECTION THRESHOLD IS 42500FC AFTER REPAIR EMBODIMENT. THE REPETITIVE INSPECTION IS TBD. THE INSPECTION METHOD IS EDDY CURRENT, ULTRASONIC IAW SRI 53-10-12-2-002-00.   MAJOR REPAIR IAW GMM 6-2-100.

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