What was found
FUSELAGE SKIN CRACKED AT FS 150.60 & STRINGER 1. CRACK ON LT SIDE OF STRINGER 1 IS .25" IN LENGTH, CRACK ON RT SIDE OF STRINGER 1 IS .65" IN LENGTH. REPAIRED IAW EO 13-1900-53-016. MAJOR REPAIR.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN CRACKED AT FS 150.60 & STRINGER 1. CRACK ON LT SIDE OF STRINGER 1 IS .25" IN LENGTH, CRACK ON RT SIDE OF STRINGER 1 IS .65" IN LENGTH. REPAIRED IAW EO 13-1900-53-016. MAJOR REPAIR.