What was found
DURING HFEC INSPECTION, FOUND CRACK AT RIGHT WING, END OF STRINGER 12 APPROXIMATELY 13.25 INCHES. REPAIR CARRIED OUT IAW SRM 57-20-00 FIG. 10 VOL I. CLIP FABRICATED AS PER FEDEX EA 1-5720-90052.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING HFEC INSPECTION, FOUND CRACK AT RIGHT WING, END OF STRINGER 12 APPROXIMATELY 13.25 INCHES. REPAIR CARRIED OUT IAW SRM 57-20-00 FIG. 10 VOL I. CLIP FABRICATED AS PER FEDEX EA 1-5720-90052.