What was found
FUSELAGE FRAME IS CRACKED IN E&E COMPT BS 380 1" INBOARD OF STR 26L ON FWD FACE OF FAIL SAFE CHORD. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE. VERIFIED REMOVAL WITH HFEC. INSTALLED REPAIR ANGLE.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE FRAME IS CRACKED IN E&E COMPT BS 380 1" INBOARD OF STR 26L ON FWD FACE OF FAIL SAFE CHORD. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE. VERIFIED REMOVAL WITH HFEC. INSTALLED REPAIR ANGLE.