What was found
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK AT TWO FASTENERS AT BS 727, STRINGER 18 IN FRAME CHORD ANGLE. REPLACED SECTION OF CHORD ANGLE, REPAIRED PER EO 5394G068. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK AT TWO FASTENERS AT BS 727, STRINGER 18 IN FRAME CHORD ANGLE. REPLACED SECTION OF CHORD ANGLE, REPAIRED PER EO 5394G068. (M)