What was found
CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 1.5 INCH CRACK THROUGH 2 FASTENER HOLES ON INNER CHORD OF FRAME BS 601, WL 208 LEFT SIDE. INSTALLED CHORD ANGLE REPAIR PER EA 66021. (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 1.5 INCH CRACK THROUGH 2 FASTENER HOLES ON INNER CHORD OF FRAME BS 601, WL 208 LEFT SIDE. INSTALLED CHORD ANGLE REPAIR PER EA 66021. (M)