What was found
FOUND CORROSION ON TOP SKIN PANEL NR 3 LT, NEAR RIB 25-28 AT T/E, OUT OF SRM LIMIT. REPAIR PERFORMED BY BLEND OUT, REPLACEMENT OF AFFECTED FASTENERS AND FLAP PEENING IAW EA 6-5720-92224 AND RAS/BAE/1001906/2005 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 NR 3 LT, NEAR RIB 25-28 AT T/E, OUT OF SRM LIMIT. REPAIR PERFORMED BY BLEND OUT, REPLACEMENT OF AFFECTED FASTENERS AND FLAP PEENING IAW EA 6-5720-92224 AND RAS/BAE/1001906/2005 ISSUE A.