What was found
FR66 Y765 CORROSION AT TOOLING MARK AND CORROSION AT SPLICE. CORROSION REMOVAL OUT OF LIMITS ORIGINAL THICKNESS 0.100" MATERIAL LOSS .04" REMAINING .06" IAW SRM 53-00-14. REMOVED AND REPLACED BEAM IAW SRM 51-72-11.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FR66 Y765 CORROSION AT TOOLING MARK AND CORROSION AT SPLICE. CORROSION REMOVAL OUT OF LIMITS ORIGINAL THICKNESS 0.100" MATERIAL LOSS .04" REMAINING .06" IAW SRM 53-00-14. REMOVED AND REPLACED BEAM IAW SRM 51-72-11.