As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
SUPPLEMENTAL INFORMATION: CRACKED WEB INBOARD OF LH WING AFT FLAP DEFLECTION ARM. MARKED WITH TAPE. APPROXIMA TE WS 281. / REMOVED CRACKED WEB; INBOARD OF L/H WING AFT. FLAP DEFLECTION ARM I.A.W. S.R.M. 51-40-02-0G-0. LOCATED AND DRILLED HOLES ON NEW WEB. PART #115A2156Y. AND SRM 51-40-05-0G-0; DRAWING #115A2156. INSTALLED WEB; I.A.W. S.R.M. 51-40-02-0G-0 AND DRAWING #115A2156.