What was found
CORROSION ON FUSELAGE SKIN AREA BELOW FILLET PANEL RUBSTRIP UPPER SECTION BETWEEN BS 760 - 800. CORROSION REMOVED IAW SRM 51-10-04 0G PAR. 26, 21, AND 15. UT WAS ACCOMPLISHED IAW NDT SPM 04-00-07 PAR 5 FIG 3 SHEET 1 AND 2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CORROSION ON FUSELAGE SKIN AREA BELOW FILLET PANEL RUBSTRIP UPPER SECTION BETWEEN BS 760 - 800. CORROSION REMOVED IAW SRM 51-10-04 0G PAR. 26, 21, AND 15. UT WAS ACCOMPLISHED IAW NDT SPM 04-00-07 PAR 5 FIG 3 SHEET 1 AND 2.