What was found
CORROSION ON INTERNAL SKIN BETWEEN FRAME 37-38, STRG 53 RT - 54 LT. REPAIR PERFORMED BY BLEND OUT, HFEC/ROTOTEST INSPECTION AND FLAP PEENING IAW EA 6-5314-82916 AND RAS/DATLS/0002629/2005 ISSUE A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CORROSION ON INTERNAL SKIN BETWEEN FRAME 37-38, STRG 53 RT - 54 LT. REPAIR PERFORMED BY BLEND OUT, HFEC/ROTOTEST INSPECTION AND FLAP PEENING IAW EA 6-5314-82916 AND RAS/DATLS/0002629/2005 ISSUE A.