What was found
CORROSION ON FUSELAGE UPPER SKIN PANEL C78-85, P4RH AND P7 LT REPAIR WAS PERFORMED BY REWORK IN SMOOTH CONTOUR AND FLAP PEENING IAW EA 6-5319-106398 AND RAS/DAHAM/4021681/2006 ISS. B
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CORROSION ON FUSELAGE UPPER SKIN PANEL C78-85, P4RH AND P7 LT REPAIR WAS PERFORMED BY REWORK IN SMOOTH CONTOUR AND FLAP PEENING IAW EA 6-5319-106398 AND RAS/DAHAM/4021681/2006 ISS. B