What was found
CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .250 INCH CRACK AT BS 887 STRINGER 9L BELT FRAME. CUTOUT DAMAGE AREA AND INSTALLED DOUBLER AND FILLER PER EA 65850. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .250 INCH CRACK AT BS 887 STRINGER 9L BELT FRAME. CUTOUT DAMAGE AREA AND INSTALLED DOUBLER AND FILLER PER EA 65850. (M)