What was found
ROA - DURING B-CHECK, VISUAL INSPECTION, FOUND .75 INCH CRACK IN FUSELAGE SKIN, BS 986.5, STR 25L. STOPPED DRILLED CRACK AND INSTALLED DOUBLER, REPAIRED PER SRM 51-30-3, FIG 1, AND SRM 53-30-3, FIG 1. (X)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
ROA - DURING B-CHECK, VISUAL INSPECTION, FOUND .75 INCH CRACK IN FUSELAGE SKIN, BS 986.5, STR 25L. STOPPED DRILLED CRACK AND INSTALLED DOUBLER, REPAIRED PER SRM 51-30-3, FIG 1, AND SRM 53-30-3, FIG 1. (X)