What was found
ROA - DURING CX-6 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK BS 727A PLUS 8 STRINGER 18L FUSELAGE SKIN. STOPPED DRILLED CRACK AND INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3 FIG 6. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
ROA - DURING CX-6 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK BS 727A PLUS 8 STRINGER 18L FUSELAGE SKIN. STOPPED DRILLED CRACK AND INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3 FIG 6. (M)