What was found
FOUND CORROSION ON TOP SKIN PANEL SECTION 19, BETWEEN FRAME 77-78, NEAR STGR 2-3 LT. REPAIR PERFORMED BY BLEND OUT CORROSION AND FLAP PEENING IAW EA 6-5319-92171 AND RAS/DATLS/0002704/2005 ISSUE A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FOUND CORROSION ON TOP SKIN PANEL SECTION 19, BETWEEN FRAME 77-78, NEAR STGR 2-3 LT. REPAIR PERFORMED BY BLEND OUT CORROSION AND FLAP PEENING IAW EA 6-5319-92171 AND RAS/DATLS/0002704/2005 ISSUE A.