What was found
DURING HFEC INSPECTION, FOUND CRACK AT LEFT WING, END OF STRINGER 44 APPROXIMATELY 1/2 INCH. REPAIR CARRIED OUT IAW SRM 57-20- 00 FIG. 10 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING HFEC INSPECTION, FOUND CRACK AT LEFT WING, END OF STRINGER 44 APPROXIMATELY 1/2 INCH. REPAIR CARRIED OUT IAW SRM 57-20- 00 FIG. 10 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.