What was found
FOUND CORROSION ON LT WING BOTTOM SKIN PANEL 2 IN THE AREA OF RIB 1-4 AROUND SEVERAL FASTENERS. REPAIR PERFORMED BY BLEND OUT CORROSION IAW EA 6-5720-101272 AND SRM 57-00-00 4.C.3(B), APPROVED BY RAS/BAE/1002868/2006 ISSUE "A".
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FOUND CORROSION ON LT WING BOTTOM SKIN PANEL 2 IN THE AREA OF RIB 1-4 AROUND SEVERAL FASTENERS. REPAIR PERFORMED BY BLEND OUT CORROSION IAW EA 6-5720-101272 AND SRM 57-00-00 4.C.3(B), APPROVED BY RAS/BAE/1002868/2006 ISSUE "A".