What was found
A .375 INCH CRACK IN FUSE SKIN AT LWR I/B CORNER OF L-4 WINDOW. INSTALLED DOUBLER PER SRM 53-30-3 F 8. C-2 TPA LETTER CHECK.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
A .375 INCH CRACK IN FUSE SKIN AT LWR I/B CORNER OF L-4 WINDOW. INSTALLED DOUBLER PER SRM 53-30-3 F 8. C-2 TPA LETTER CHECK.