What was found
PUNCTURE ON CUSP WEB BS 169 AND X 50. HFEC INSPECTION WAS ACCOMPLISHED AFTER TRIM OUT, AND NO CRACKS WERE FOUND IAW NDT SPM 06-10-01. REPAIRED IAW SRM 51-70-10 REPAIR 2 FIG. 201.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
PUNCTURE ON CUSP WEB BS 169 AND X 50. HFEC INSPECTION WAS ACCOMPLISHED AFTER TRIM OUT, AND NO CRACKS WERE FOUND IAW NDT SPM 06-10-01. REPAIRED IAW SRM 51-70-10 REPAIR 2 FIG. 201.