What was found
CORROSION ON MILLED FRAME 63A BETWEEN STRG 32-35 AND STRG 39-41 RT. REPAIR PERFORMED BY SMOOTH BLEND OUT, HFEC INSPECTION FOR NIL FINDINGS AND FLAP PEENING IAW EA 6-5317-82874 AND RAS/DAHAM/4019554/2005 ISSUE A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CORROSION ON MILLED FRAME 63A BETWEEN STRG 32-35 AND STRG 39-41 RT. REPAIR PERFORMED BY SMOOTH BLEND OUT, HFEC INSPECTION FOR NIL FINDINGS AND FLAP PEENING IAW EA 6-5317-82874 AND RAS/DAHAM/4019554/2005 ISSUE A.