As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
REMOVE INBD FLAP HINGE FITTING FOR LT WING OTBD FLAP TO DETERMINE CRACK LENGTH. FLAP FITTING IS LOCATED ON AFT WING SPAR BS 164. MEASURED AND MARKED ENDS OF CRACK IAW NDTSPM 06-10-01.001. CRACK MEASURES .625 IN LENGTH. INSTALLATION OF INBD FLAP FITTING TO BE ACCOMPLISHED ON NR NR 15. REPAIR OF CRACK TO BE ACCOMPLISHED ON NR 1, PRI 544925-14AD.