What was found
FUSELAGE LEFT AFT DOOR X-RAY SHOWED CRACK AT THE LOWER FORWARD CORNER OF DOOR CUTOUT. CUTOUT CRACKED 3.8125 INCHES SECTION AND INSTALLED REPAIR IAW DC-8 SRM 53-2-0, 51-1-21 AND 51-1-20.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE LEFT AFT DOOR X-RAY SHOWED CRACK AT THE LOWER FORWARD CORNER OF DOOR CUTOUT. CUTOUT CRACKED 3.8125 INCHES SECTION AND INSTALLED REPAIR IAW DC-8 SRM 53-2-0, 51-1-21 AND 51-1-20.