What was found
ROA - DURING CX-6 CHECK VISUAL/EDDY CURRENT INSPECTION, FOUND .625 INCH CRACK BS 945 STRINGER 24L FUSELAGE SKIN. REMOVED CRACK AND INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3 FIG 3. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
ROA - DURING CX-6 CHECK VISUAL/EDDY CURRENT INSPECTION, FOUND .625 INCH CRACK BS 945 STRINGER 24L FUSELAGE SKIN. REMOVED CRACK AND INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3 FIG 3. (M)