What was found
FUSELAGE FRAME CRACKED BELOW CABIN FLOOR, OVER WING SECTION BS 616 RT SIDE. MAJOR REPAIR ACP'D. REMOVED DAMAGE AND VERIFIED WITH HFEC. INSTALLED A FILLER AND A REPAIR ANGLE PER MM 53-11-89-801.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE FRAME CRACKED BELOW CABIN FLOOR, OVER WING SECTION BS 616 RT SIDE. MAJOR REPAIR ACP'D. REMOVED DAMAGE AND VERIFIED WITH HFEC. INSTALLED A FILLER AND A REPAIR ANGLE PER MM 53-11-89-801.