As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT WING FORWARD SPAR IS CORRODED AT BONDING STRAP LOCATION FOR NUMBER 1 FUEL FWD BOOST PUMP. / REMOVED CORROSION ON LH WING FWD SPAR WEB AT THE BONDING STRAP ATTACH POINT IAW SRM 51-10-02-0G-0. VERIFIED ALLOWABLE LIMITS; ORIGINAL .485' LOSS .126' REMIANING .359'; OUT OF LIMITS IAW SRM 57-20-10-1A-3. REPAIRED FWD SPAR WEB AT BONDING STRAP ATTACH POINT IAW EA 190728 IR AND SWA EA 1-757-16538 REV IR.