# SDR FDEA201605261735

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: May 26, 2016
- Submitted: May 26, 2016
- Operation: Air carrier
- Aircraft: [N746FD](https://openairdocs.org/aircraft/N746FD), 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: 688
- Aircraft time: 55,882 hours, 20,753 cycles
- System (JASC): [5311 · Fuselage Main, Frame](https://openairdocs.org/jasc/5311)
- Part: Fitting
- Part number: A53812308201
- Condition: Cracked
- Location: Fuselage
- Stage of operation: IN
- How discovered: O
- Nature of condition: O
- Precautionary procedure: K
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/FDEA201605261735

## Discrepancy

FUSELAGE INTERNAL STRUCTURE, BETWEEN FRAME 41 TO 46, FROM STRINGER 24R TO 28R, NDT CHECK FOUND ONE HOLE WITH CRACK SIGNAL AT FRAME 42, STRINGER 25R - 26R LOCATION, THE FIRST HOLE FROM UP TO DOWN.  PERFORMED BUSHES INSTALLATION REPAIR IAW EA6-5315-T0325510, PT1 EA.  TITLE: FUSELAGE-FRAME FOOT-CRACKS, FRAME FEET ATTACHMENT HOLES "H1" ON FRAME 42, 43, 44, RT SIDE BETWEEN STR 25R TO STR 27R.  THIS WAS CATEFORY "C" REPAIR, REPAIR, LIFE LIMITATION WAS 6 MONTHS.  THIS WAS A MAJOR REPAIR IAW GMM6-2-100.

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