What was found
CLT - INSPECTION FOUND BY ULTRASONIC AND EDDY CURRENT, A CRACK APPROXIMATELY 1 INCH, LOCATED AT THE FUSELAGE CHORD, RHS BS 727, OUTBOARD AT STRINGER 18A. CHORD SECTION REPLACED AS PER EO 5394G068, EO 5394G6075 AND SB 737-53-1088. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CLT - INSPECTION FOUND BY ULTRASONIC AND EDDY CURRENT, A CRACK APPROXIMATELY 1 INCH, LOCATED AT THE FUSELAGE CHORD, RHS BS 727, OUTBOARD AT STRINGER 18A. CHORD SECTION REPLACED AS PER EO 5394G068, EO 5394G6075 AND SB 737-53-1088. (M)