What was found
SJO - OBSERVED DURING FUSELAGE SKIN REPLACEMENT, LEVEL 2 CORROSION, STRINGER 24 LEFT, BS 1010. DEFECT SIZE 1.5 INCHES. ACCOMPLISHED STRINGER REPAIR IAW 53-10-03 FIG 1. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
SJO - OBSERVED DURING FUSELAGE SKIN REPLACEMENT, LEVEL 2 CORROSION, STRINGER 24 LEFT, BS 1010. DEFECT SIZE 1.5 INCHES. ACCOMPLISHED STRINGER REPAIR IAW 53-10-03 FIG 1. (M)