What was found
HFEC OPEN HOLE INSPECTION FOUND TWO HOLES WITH CRACK INDICATION ON FUSELAGE CTR SECTION FRAME 54, STRINGER 44L LATERAL PANEL.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
HFEC OPEN HOLE INSPECTION FOUND TWO HOLES WITH CRACK INDICATION ON FUSELAGE CTR SECTION FRAME 54, STRINGER 44L LATERAL PANEL.