What was found
AT D-CHECK, FOUND FUSELAGE INTERIOR FRAME CRACKED AT BS 600, INNER FLANGE ABOVE FLOOR LEVEL. CUT OUT DAMAGED AREA, INSTALLED REPAIR PER SRM 53-10-4. REPAIR, 8 INCHES BY 10.5 INCHES.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AT D-CHECK, FOUND FUSELAGE INTERIOR FRAME CRACKED AT BS 600, INNER FLANGE ABOVE FLOOR LEVEL. CUT OUT DAMAGED AREA, INSTALLED REPAIR PER SRM 53-10-4. REPAIR, 8 INCHES BY 10.5 INCHES.