What was found
A .125 INCH CRACK AT FUSE SKIN AT L-1 WINDOW UPPER O/B CORNER. INSTALLED DOUBLER PER SRM 53-30-3 REPAIR II FIG 11.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
A .125 INCH CRACK AT FUSE SKIN AT L-1 WINDOW UPPER O/B CORNER. INSTALLED DOUBLER PER SRM 53-30-3 REPAIR II FIG 11.