As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RT WING FRONT SPAR UPPER FWD CHORD AT STA OSS 456.98 HAS CORROSION. REMOVED CORROSION FROM UPPER FWD CHORD AT RT WING FRONT SPAR, STA OSS 456.98 IAW SRM 51-10-02 PAGE 12-13. THICKNESS FOUND, MAX: 0.078 INCH, MIN: 0.055 INCH. NO CRACKS FOUND. BLENDING LIMITS ON THE UPPER SKIN, LEADING EDGE SPLICE PLATE ACCEPTED AS PERMANENT REPAIR IAW MFG SERVICE REQUEST 1-499965626. FAA FORM 8100-9 WILL BE ISSUED APPROVING THIS REPAIR.