What was found
UPON REMOVAL OF STRINGER 22R BETWEEN FS 333.00-349.00 CORROSION WAS FOUND ON INTERNAL FUSELAGE SKIN. REPAIRED IAW MHIRJ REO 670-53-21-2448 REV-- DATED 2024-08-16
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
UPON REMOVAL OF STRINGER 22R BETWEEN FS 333.00-349.00 CORROSION WAS FOUND ON INTERNAL FUSELAGE SKIN. REPAIRED IAW MHIRJ REO 670-53-21-2448 REV-- DATED 2024-08-16