What was found
DURING HFEC SURFACE INSPECTION, FOUND CRACK APPROX 1/2 INCH AT RT FUSELAGE SKIN BS 395 STR-7R. CRACK REPAIRED PER SRM 53-00-01 REPAIR 1, FIGURE 201.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING HFEC SURFACE INSPECTION, FOUND CRACK APPROX 1/2 INCH AT RT FUSELAGE SKIN BS 395 STR-7R. CRACK REPAIRED PER SRM 53-00-01 REPAIR 1, FIGURE 201.