What was found
ROA - DURING CX-6 CHECK VISUAL/EDDY CURRENT INSPECTION, FOUND .75 INCH CRACK AND .25 INCH CRACK BS 727A PLUS 8 INCHES STRINGER 18L FUSELAGE SKIN. INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3. (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 .75 INCH CRACK AND .25 INCH CRACK BS 727A PLUS 8 INCHES STRINGER 18L FUSELAGE SKIN. INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3. (M)