What was found
CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A ..1 INCH CRACK AT BS 726 STRINGER 18A RIGHT CHORD ANGLE. INSTALLED NEW PART PER EA 65273A. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A ..1 INCH CRACK AT BS 726 STRINGER 18A RIGHT CHORD ANGLE. INSTALLED NEW PART PER EA 65273A. (M)