What was found
CLT - DURING C-4 CHECK VISUAL INSPECTION, FOUND A CRACK IN RADIUS OF FUSELAGE FRAME STATION 720, BL 0 BELOW ACE LOADER JACK SCREW ASSY. INSTALLED REPAIR ANGLE PER SRM 51-70-11. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CLT - DURING C-4 CHECK VISUAL INSPECTION, FOUND A CRACK IN RADIUS OF FUSELAGE FRAME STATION 720, BL 0 BELOW ACE LOADER JACK SCREW ASSY. INSTALLED REPAIR ANGLE PER SRM 51-70-11. (M)