What was found
HFEC INSPECTION FOUND 01EA CRACK APPROX 0.250" IN LENGTH ON THE FUSELAGE SKIN AROUND THE 9TH STRINGER-ATTACH RIVET ALONG S-14AR, AFT OF FRAME 1629. REPAIRED PER SRM 53-80-01. (LP 0913918)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
HFEC INSPECTION FOUND 01EA CRACK APPROX 0.250" IN LENGTH ON THE FUSELAGE SKIN AROUND THE 9TH STRINGER-ATTACH RIVET ALONG S-14AR, AFT OF FRAME 1629. REPAIRED PER SRM 53-80-01. (LP 0913918)