What was found
HFEC INSPECKTION FOUND ONE CRACK APPROX 0.275 INCHES IN LENGTH ON THE FUSELAGE SKIN, BELOW THE 11TH FASTENER 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 INSPECKTION FOUND ONE CRACK APPROX 0.275 INCHES IN LENGTH ON THE FUSELAGE SKIN, BELOW THE 11TH FASTENER AT STRINGER 13AR, FROM FWD TO AFT, BETWEEN BS 1654.5 AND 1678. REPAIRED IAW SRM 53-80-01.