What was found
UPPER FUSELAGE MAIN CABIN WING CENTER SECTION AT BS 825.95 LBL50 WL204 STUB BEAM WEB CRACKED. REPAIRED FUSELAGE WEB SECTION AT BS 825.95 FROM LBL 49 TO LBL 57 IAW EO COO-2-53-274-08 DTD 9/16/08 DOCUMENTED ON FAA FORM 8110-3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
UPPER FUSELAGE MAIN CABIN WING CENTER SECTION AT BS 825.95 LBL50 WL204 STUB BEAM WEB CRACKED. REPAIRED FUSELAGE WEB SECTION AT BS 825.95 FROM LBL 49 TO LBL 57 IAW EO COO-2-53-274-08 DTD 9/16/08 DOCUMENTED ON FAA FORM 8110-3.