What was found
A .25 INCH CRACK FUSELAGE SKIN AT FASTENER JUST AFT OF L-3 COCKPIT WINDOW. REPAIRED PER SRM 53-30-3 FIG 8.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
A .25 INCH CRACK FUSELAGE SKIN AT FASTENER JUST AFT OF L-3 COCKPIT WINDOW. REPAIRED PER SRM 53-30-3 FIG 8.