What was found
BULGING EVIDENT ON WING CENTER SECTION REAR SPAR WEB AT BS 870, 3RD VERTICAL STIFFENER FROM LEFT SIDE. CORROSION FOUND ON VERTICAL STIFFENER AT LBL 24.70. STIFFENER REPLACED IAW SRM 51-30-2 AND DRAWING 65-16202.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
BULGING EVIDENT ON WING CENTER SECTION REAR SPAR WEB AT BS 870, 3RD VERTICAL STIFFENER FROM LEFT SIDE. CORROSION FOUND ON VERTICAL STIFFENER AT LBL 24.70. STIFFENER REPLACED IAW SRM 51-30-2 AND DRAWING 65-16202.