What was found
E/E BAY INTERIOR FUSELAGE SKIN AT BS 395-418, BETWEEN STRINGER 25-26R, CORRODED. FOUND CORROSION OUT OF LIMITS IAW SRM 53-00-01, PG.104, FIG 101, DETAIL II. COMPLIED WITH EA F-5330-T0300227. MAJOR REPAIR.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
E/E BAY INTERIOR FUSELAGE SKIN AT BS 395-418, BETWEEN STRINGER 25-26R, CORRODED. FOUND CORROSION OUT OF LIMITS IAW SRM 53-00-01, PG.104, FIG 101, DETAIL II. COMPLIED WITH EA F-5330-T0300227. MAJOR REPAIR.