What was found
GSO - INSPECTION FOUND A .25 INCH CRACK IN SKIN AT FASTENER HOLE, BS 580, LAP SEAM 26L. THE DAMAGED AREA WAS REMOVED AND REPAIRED. DOUBLER, FILLER, AND SHIM WERE INSTALLED IAW SRM 53-30-3 AND SRM 51-30-2. (X)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
GSO - INSPECTION FOUND A .25 INCH CRACK IN SKIN AT FASTENER HOLE, BS 580, LAP SEAM 26L. THE DAMAGED AREA WAS REMOVED AND REPAIRED. DOUBLER, FILLER, AND SHIM WERE INSTALLED IAW SRM 53-30-3 AND SRM 51-30-2. (X)