What was found
UPPER FUSELAGE AT BS 1016, LBL40 FLOOR WEB CRACKED. CRACK IN THE AFT CABIN STRESS WEB. FABRICATED AND INSTALLED REPLACEMENT WEB IAW DWG 65-46812 AND SRM R108.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
UPPER FUSELAGE AT BS 1016, LBL40 FLOOR WEB CRACKED. CRACK IN THE AFT CABIN STRESS WEB. FABRICATED AND INSTALLED REPLACEMENT WEB IAW DWG 65-46812 AND SRM R108.