What was found
FOUND AFT CARGO DOOR PAN CHAFED THROUGH AT AFT EDGE ABOVE LOCKING CAM AND NR 1 BEAM AFT TEE CRACKED 1.5 INCHES LENGTH. MAINTENANCE INSTALLED REPAIR TO DOOR PAN IAW SRM 52-05 FIG 26. INSTALLED DOUBLER ANGLE REPAIR IAW SRM 52-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FOUND AFT CARGO DOOR PAN CHAFED THROUGH AT AFT EDGE ABOVE LOCKING CAM AND NR 1 BEAM AFT TEE CRACKED 1.5 INCHES LENGTH. MAINTENANCE INSTALLED REPAIR TO DOOR PAN IAW SRM 52-05 FIG 26. INSTALLED DOUBLER ANGLE REPAIR IAW SRM 52-01.