What was found
CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT LOWER FASTENER HOLE INNER CHORD ANGLE BS 616 FUSELAGE FRAME WL 200 LEFT SIDE. INSTALLED DOUBLER PER EA 65335. (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 INCH CRACK AT LOWER FASTENER HOLE INNER CHORD ANGLE BS 616 FUSELAGE FRAME WL 200 LEFT SIDE. INSTALLED DOUBLER PER EA 65335. (M)