What was found
INTERNAL FUSELAGE SKIN AT FRAME 35, STRINGER 30R, HAD A CRACK INDICATION. INTERIM REPAIR ACCOMPLISHED IAW ECRA 5330-0620 5 PART 1.
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. INTERIM REPAIR ACCOMPLISHED IAW ECRA 5330-0620 5 PART 1.