# SDR FDEA202606180929

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: June 18, 2026
- Submitted: July 16, 2026
- Operation: Air carrier
- Aircraft: [N680FE](https://openairdocs.org/aircraft/N680FE), 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: 794
- Aircraft time: 35,313 hours, 20,174 cycles
- System (JASC): [5753 · Trailing Edge Flaps](https://openairdocs.org/jasc/5753)
- Part: Flap
- Part number: A5796030000351
- Part serial: FH1241
- Condition: Cracked
- Location: Zone 600
- Stage of operation: IN
- How discovered: X
- Nature of condition: O
- Precautionary procedure: K
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/FDEA202606180929

## Discrepancy

RH WING CENTER FLAP FOUND 1EA CRACK AT RIB26 FIRST FASTENER BETWEEN STGR2.7 AND   STGR2.8 COMPLIED WITH EA 6-5750-T0362465 A P2, EA TITLE: WING - FLIGHT SURFACES - RH CENTER FLAP,   CRACK IN UPPER FLANGE OF RIB 26 & 27. REMOVED THE EXISTING DOUBLER ON BOTTOM SKIN   BETWEEN RIB26 AND RIB27, STGR2.1 AND REAR SPAR.  REPAIRED RH WING CENTER FLAP RIB26   UPPER FLANGE BETWEEN STGR2.7 AND STGR2.8. INSTALLED REPAIR DOUBLER ON BOTTOM SKIN   BETWEEN RIB26 AND RIB27, STGR2.2 AND REAR SPAR  THIS REPAIR CATEGORY A.  MAJOR REPAIR   IAW FEDEX GMM6-2-100. SEE WRI 57505019 FOR WORK DETAILS.

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