What was found
HFEC INSPECTION FOUND ONE CRACK, APPROXIMATELY .0-275" IN LENGTH ON THE FUSELAGE SKIN BELOW AT STRINGER 13AR, FROM FWD TO AFT , BETWEEN BS 1654.5 AND 1678. REPAIRED IAW SRM 53-80-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
HFEC INSPECTION FOUND ONE CRACK, APPROXIMATELY .0-275" IN LENGTH ON THE FUSELAGE SKIN BELOW AT STRINGER 13AR, FROM FWD TO AFT , BETWEEN BS 1654.5 AND 1678. REPAIRED IAW SRM 53-80-01.