What was found
A .5 INCH CRACK FUSELAGE SKIN AT L-4 WINDOW I/B FWD ATTACH SCREW. REPAIRED PER SRM 53-30-3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
A .5 INCH CRACK FUSELAGE SKIN AT L-4 WINDOW I/B FWD ATTACH SCREW. REPAIRED PER SRM 53-30-3.