What was found
AT C-CHECK, FOUND CRACK IN TIE FITTING, INTERIOR STRUCTURE OF FUSELAGE, UPPER LOBE, FS 950 STRINGER 4R. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AT C-CHECK, FOUND CRACK IN TIE FITTING, INTERIOR STRUCTURE OF FUSELAGE, UPPER LOBE, FS 950 STRINGER 4R. (M)