What was found
DURING INSP OF FUSELAGE FOUND CORROSION WITH A CRACK, CRACK APPROX 3/8 IN LENGTH REPAIRED IAW SRM 53-60-01 FIG 201 REPAIR 2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING INSP OF FUSELAGE FOUND CORROSION WITH A CRACK, CRACK APPROX 3/8 IN LENGTH REPAIRED IAW SRM 53-60-01 FIG 201 REPAIR 2.