What was found
VERTICAL CRACK INDICATION NOTED ON INTERIOR FUSELAGE SKIN AT FS 640 AND STR 10L APPROX 0.125 AFT OF UPPER SKIN CUTOUT AND 1.437 INCH IN LENGTH. FAILED NDT INSPECTION AT 100 FSH.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
VERTICAL CRACK INDICATION NOTED ON INTERIOR FUSELAGE SKIN AT FS 640 AND STR 10L APPROX 0.125 AFT OF UPPER SKIN CUTOUT AND 1.437 INCH IN LENGTH. FAILED NDT INSPECTION AT 100 FSH.