What was found
CORROSION ON INNER FUSELAGE SKIN AT FRAME 364 & STRINGER 26R. REMOVED CORROSION, REMAINING MATERIAL OUT OF LIMITS, FABRICATED AND INSTALLED SHIM IAW REO 670-53-1290 DATED 4 21 16 & SRM 53-21-01 & 53-00-00. NDT PERFORMED.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CORROSION ON INNER FUSELAGE SKIN AT FRAME 364 & STRINGER 26R. REMOVED CORROSION, REMAINING MATERIAL OUT OF LIMITS, FABRICATED AND INSTALLED SHIM IAW REO 670-53-1290 DATED 4 21 16 & SRM 53-21-01 & 53-00-00. NDT PERFORMED.