What was found
CHAFING DAMAGE (10 BY 1.5 MM) ON PYLON REINFORCING PLATE, RT WING AT FWD OUTBOARD EDGE, RIB 9. REPAIR PERFORMED BY BLEND OUT AND NDT INSPECTION IAW EA 6-5720-95909 AND RAS/BAE/1002261/2006.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CHAFING DAMAGE (10 BY 1.5 MM) ON PYLON REINFORCING PLATE, RT WING AT FWD OUTBOARD EDGE, RIB 9. REPAIR PERFORMED BY BLEND OUT AND NDT INSPECTION IAW EA 6-5720-95909 AND RAS/BAE/1002261/2006.