What was found
DURING INSPECTION FOUND A CRACK AT FUSELAGE STA 1760 1.25 INCH IN LENGTH. INSTALLED REPAIR PER SRM 53-2-1 ITEM 16.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING INSPECTION FOUND A CRACK AT FUSELAGE STA 1760 1.25 INCH IN LENGTH. INSTALLED REPAIR PER SRM 53-2-1 ITEM 16.