What was found
FUSELAGE SKIN CRACKED AT BS 940, JUST BELOW STRINGER 24R, VERIFIED WITH HFEC. INSTALLED REPAIR IAW DWG 5330D1816, SHEET 1-2 AND SRM 53-30-3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN CRACKED AT BS 940, JUST BELOW STRINGER 24R, VERIFIED WITH HFEC. INSTALLED REPAIR IAW DWG 5330D1816, SHEET 1-2 AND SRM 53-30-3.