As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
-AD- FOUND CRACK INDICATION OF L/H INBOARD FLAP FORWARD HINGE SUPPORT FITTING #8 OPEN BUSHING HOLE DURING BHEC PER PRI 622950-14AD (REV 1) STEP 12 QC2013. REINSPECTED INBD FLAP HINGE SUPPORT FITTING #8 BHEC INSPECTION IAW NDTSPM PY6 06-10-01-003 NO CRACK INDICATIONS NOTED QC5158. (LP #0713987)