What was found
LEFT FUSELAGE FRAME AT BS 235 HAS AN INDICATIONN. A THREE INCH LONG CRACK PROJECTING FROM THE RADIUS OF FRAME AT STRINGER 13L.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT FUSELAGE FRAME AT BS 235 HAS AN INDICATIONN. A THREE INCH LONG CRACK PROJECTING FROM THE RADIUS OF FRAME AT STRINGER 13L.