# SDR FDEA201209293514

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: September 29, 2012
- Submitted: October 1, 2012
- Operation: Air carrier
- Aircraft: [N660FE](https://openairdocs.org/aircraft/N660FE), registered now
- Make and model: Airbus A300 B4-622R
- Registry model: [Airbus A300 B4-622R](https://openairdocs.org/model/airbus-a300-b4-622r) (OpenAirDocs)
- Aircraft serial: 759
- Aircraft time: 24,289 hours, 13,074 cycles
- System (JASC): [5340 · Fuselage Main, Attach Fittings](https://openairdocs.org/jasc/5340)
- Part: Fitting
- Part number: A5711109220300
- Condition: Cracked
- Location: Zone 100
- 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/FDEA201209293514

## Discrepancy

ANGLE FITTING ON REAR SPAR AND FRAME 47R INBD OF WING RIB 1, FOUND HOLE "H" TO BE  CRACKED WHEN ROTO PROBE WAS PERFORMED TO SATISFY AD 2005-23-08.  STEP REAMED HOLE "H" FROM .381" TO .436" IAW EO 6-5310-7-3319 B2 PT 3.  ROTO PROBED  HOLE IAW NTM 57-10-50, PART 6 PROCEDURE A.  VERIFIED CRACK REMOVED.

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