What was found
FUSELAGE INTERNAL STRUCTURE AT FRAME 46, STGR 24-28LT FRAME FOOT INBD ROW LOWER NR 2 FASTENER HOLE FOUND CRACK SIGNAL.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE INTERNAL STRUCTURE AT FRAME 46, STGR 24-28LT FRAME FOOT INBD ROW LOWER NR 2 FASTENER HOLE FOUND CRACK SIGNAL.