As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
IAW EO F-2822-7-5009 PART 3, STEP B1. C (PAGE 16 OF 33). CORROSION AT RT AFT WING SPAR SURFACE. REMOVED AND SPAR WEB THICKNESS FOUND LESS THAN THE MINIMUM. IAW EO F-2822-7-5009, PART 3, STEP B1. C (PAGE 16 OF 33). CORROSION AT RT AFT WING SPAR SURFACE REMOVED AND SPAR WEB THICKNESS FOUND LESS THAN THE MINIMUM. CORROSION REPAIRED IAW EA F-5710-162930, PART 1. MAJOR REPAIR.