As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION ON ANGLE THAT ATTACH FUSELAGE TO CUSP ANGLE BTW LONGS 18L-19L, BTW STA Y=889-908. ANGLE WAS REPLACED PER SRM 53-20-51-01 AND DWG 9910151 ITEM -117. MEASURED (UT) WAS ACCOMPLISHED PER NDT SPM 04-00-07 PAR 5 FIG 3 SHEET 1 AND 2. THE ORIGINAL THICKNESS ON CUSP ANGLE LT IS .080" AND REMAINING THICKNESS .054 ",THEREFORE OUTSIDE LIMITS PER SRM 53-00-00-1A FIG 103 SHEET 1.