What was found
INTERNAL FUSELAGE SKIN AT FRAME 35, STRINGER 30R, HAD A CRACK INDICATION. ACCOMPLISHED A PERMANENT REPAIR IAW PART 3, ECRA 5331-02229.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INTERNAL FUSELAGE SKIN AT FRAME 35, STRINGER 30R, HAD A CRACK INDICATION. ACCOMPLISHED A PERMANENT REPAIR IAW PART 3, ECRA 5331-02229.