What was found
FUSELAGE DAMAGE BETWEEN BS 1031 AND 1051 BETWEEN STRINGERS 21 - 27R. BLENDED IAW SRM 51-12-00 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-61-01. T MAJOR REPAIR IAW GMM 5-3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE DAMAGE BETWEEN BS 1031 AND 1051 BETWEEN STRINGERS 21 - 27R. BLENDED IAW SRM 51-12-00 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-61-01. T MAJOR REPAIR IAW GMM 5-3.