What was found
CLT - DURING Q-4 CHECK, FOUND FUSELAGE FRAME CRACKED .200 INCH IN LENGTH, THREE (3) HOLES AT CLIP ATTACH ON FRAME. REMOVED DAMAGE AND INSTALLED DOUBLER PER SRM 53-00-07, AND EA 64581. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CLT - DURING Q-4 CHECK, FOUND FUSELAGE FRAME CRACKED .200 INCH IN LENGTH, THREE (3) HOLES AT CLIP ATTACH ON FRAME. REMOVED DAMAGE AND INSTALLED DOUBLER PER SRM 53-00-07, AND EA 64581. (M)