As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
L/H WING FWD SPAR BOOST PUMP UPPER ANGLE IS CORRODED / REMOVED CORROSION FROM LH WING FWD SPAR BOOST PUMP; 50% MATERIAL LOSS FOUND OUT OF LIMITS IAW SRM 51-10-02-0G-0. LOCATED; DRILLED; AND INSTALLED NEW ANGLE IAW DWG 112A2004 REV. A RESTORED CIC IAW AMM 51-21-91-620-802