# SDR FDEA201606172028

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: June 17, 2016
- Submitted: June 17, 2016
- Operation: Air carrier
- Aircraft: [N726FD](https://openairdocs.org/aircraft/N726FD), 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: 575
- Aircraft time: 50,512 hours, 25,964 cycles
- System (JASC): [5311 · Fuselage Main, Frame](https://openairdocs.org/jasc/5311)
- Part: Fitting
- Part number: A57111016203
- Condition: Cracked
- Location: Fuselage
- Stage of operation: IN
- How discovered: E
- Nature of condition: O
- Precautionary procedure: K
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/FDEA201606172028

## Discrepancy

FUSELAGE INTERNAL STRUCTURE AT FRAME 41, STR 24-28 RT FRAME FOOT INBD ROW UPR NR 1 FASTENER HOLE FOUND CRACKED SIGNAL.  REPAIRED THE CRACKED HOLE OF FUSELAGE INTERNAL STRUCTURE AT FRAME 41, STR 24-28, RT FRAME FOOT INBD ROW UPPER NR 1 FASTENER IAW EA 6-5315-T0326077 P1. TITLE: FUSELAGE, FRAME, FOOT CRACKS, FRAME FEET ATTACHMENT HOLES AT RT SIDE FRAME 41-43 AND LT SIDE FRAME 46.  THIS REPAIR CATEGORY IS C.  REPAIR LIFE LIMITATION IS 6 MONTHS.  MAJOR REPAIR IAW GMM 6-2-100.

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