What was found
CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT LOWER FAST HOLE INNER CHORD ANGLE BS 601 FUSELAGE FRAME, WL 203 LEFT SIDE. INSTALLED DOUBLER PER EA 65335 AND TR 53-10-23. (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 FAST HOLE INNER CHORD ANGLE BS 601 FUSELAGE FRAME, WL 203 LEFT SIDE. INSTALLED DOUBLER PER EA 65335 AND TR 53-10-23. (M)