# SDR 08FDEA03292

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: August 6, 2008
- Submitted: August 12, 2008
- Operation: Air carrier
- Aircraft: [N664FE](https://openairdocs.org/aircraft/N664FE), 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: 768
- Aircraft time: 19,142 hours, 10,216 cycles
- System (JASC): [5311 · Fuselage Main, Frame](https://openairdocs.org/jasc/5311)
- Part: Frame
- Part number: A5381231020001
- 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/08FDEA03292

## Discrepancy

FRAME 44 FROM STRINGER 25L TO STRINGER 26L, FASTENER HOLE "B" AS CALLED OUT IN EO E6-5310-7-5006 PT1 STEP 70 STILL SHOWS A CRACK INDICATION AFTER REAMING IT TO A MAX SIZE OF 0.437.  REMOVED FRAME 44 SECTION FROM S22-27L IAW SRM 51-40-21, PARA 'S 6 AND 7.  RECEIVED NEW FRAME SECTION P/N A5381231020001.  LOCATED AND DRILLED NEW FRAME 44 SECTION REFERENCING DWG A53812304, REV "A" AND SRM 51-40-21, PARA'S 6 AND 7.

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