What was found
AFW - FUSELAGE FRAME INNER CHORD HAS CORROSION REMOVAL ON LOWER SURFACE AS SHOWN MATERIAL REMAINING IS BEYOND SRM 53-00-07-1 LIMITS. BLENDED CORROSION IAW MRB 767-1816 DATED FEB 09, 1999. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AFW - FUSELAGE FRAME INNER CHORD HAS CORROSION REMOVAL ON LOWER SURFACE AS SHOWN MATERIAL REMAINING IS BEYOND SRM 53-00-07-1 LIMITS. BLENDED CORROSION IAW MRB 767-1816 DATED FEB 09, 1999. (M)