As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT WING INBD FLAP OTBD EDGE CENTER WEB FOUND CRACKED. CRACKED WEB REMOVED AS PER SRM 51-35-01 REVISION 50. NEW WEB FABRICATED IAW DRAWING ARC2305 REVISION C. NEW FABRICATED WEB INSTALLED IAW SRM 51-35-01 REVISION 50 AND EA 1-5750-163519. FLAP OPS TEST CARRIED OUT IAW AMM 27-50-00-860-801 REVISION 74 AND FOUND SATISFACTORY. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115.