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 RT SIDE. INSTALLED REPAIR DOUBLER AND HI-LOCKS PER TR 53-10-23, EA 65335 AND SRM 53-60-07. (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 RT SIDE. INSTALLED REPAIR DOUBLER AND HI-LOCKS PER TR 53-10-23, EA 65335 AND SRM 53-60-07. (M)