What was found
EXFOLIATION CORROSION - SKIN CTR WING Y=1226~1239 X=-42~-97 WING TANK UPPER SURFACE TOTAL:39 AREA. REPAIRED THE CORROSION AREA IAW EGAT EI W2009A57B-1378 REV 00.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
EXFOLIATION CORROSION - SKIN CTR WING Y=1226~1239 X=-42~-97 WING TANK UPPER SURFACE TOTAL:39 AREA. REPAIRED THE CORROSION AREA IAW EGAT EI W2009A57B-1378 REV 00.