What was found
FOUND CRACK ON STIFFENER AT FRAME 12A LT, STRG 27. REPLACEMENT OF STIFFENER AS PER DWG A536-10318/SH 05.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FOUND CRACK ON STIFFENER AT FRAME 12A LT, STRG 27. REPLACEMENT OF STIFFENER AS PER DWG A536-10318/SH 05.