What was found
CORROSION ON FAIL/SAFE RING PAX DOOR NR 1 LT FUSELAGE SKIN PANEL AT FRAME 16A, AFT UPPER CORNER. REPAIR PERFORMED BY BLENDING CORROSION AND HFEC INSPECTION IN THE AREA IAW EA 6-5312-82849 AND RAS/036735/006/2005 ISSUE A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CORROSION ON FAIL/SAFE RING PAX DOOR NR 1 LT FUSELAGE SKIN PANEL AT FRAME 16A, AFT UPPER CORNER. REPAIR PERFORMED BY BLENDING CORROSION AND HFEC INSPECTION IN THE AREA IAW EA 6-5312-82849 AND RAS/036735/006/2005 ISSUE A.