What was found
DURING INSPECTON, FOUND CORROSION LT WING, BOTTOM SKIN PANEL NR 1 BETWEEN RIBS 7-8 FWD OF SPAR. AREAS 1 =110 MML X 70MMW X 8.87 WWD, AREAS 2 = 60 MML X 65 MML X 8.87 MMD.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING INSPECTON, FOUND CORROSION LT WING, BOTTOM SKIN PANEL NR 1 BETWEEN RIBS 7-8 FWD OF SPAR. AREAS 1 =110 MML X 70MMW X 8.87 WWD, AREAS 2 = 60 MML X 65 MML X 8.87 MMD.