What was found
A .375 INCH CRACK IN FUSELAGE SKIN JUST AFT OF R-3 WINDOW. INSTALLED DOUBLER PER SRM 53-03-3 FIG 8, IV.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
A .375 INCH CRACK IN FUSELAGE SKIN JUST AFT OF R-3 WINDOW. INSTALLED DOUBLER PER SRM 53-03-3 FIG 8, IV.