What was found
FUSELAGE BS 727, STRINGER 18A LEFT OUTBOARD CHORD DETECTED CRACK BY METHOD OF HFEC INSPECTION. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE BS 727, STRINGER 18A LEFT OUTBOARD CHORD DETECTED CRACK BY METHOD OF HFEC INSPECTION. (M)