What was found
RIGHT FUSELAGE DENTED BETWEEN BS 1053-1076. STRINGERS 22-23R. ACCOMPLISHED HFEC IAW NDT SPM 06-10-01.001. NO CRACKS NOTED.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RIGHT FUSELAGE DENTED BETWEEN BS 1053-1076. STRINGERS 22-23R. ACCOMPLISHED HFEC IAW NDT SPM 06-10-01.001. NO CRACKS NOTED.