As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE:C1 WHILE ACCOMPLISHMENT OF MCD FWD HINGE REPLACEMENT AFTER REMOVAL OF THE ACTUATOR CLOSE OUT PNL FOUND A 1" CRACK ON THE FWD UPPER MAIN FRAME CRACK ON "Z" FRAME STOPPED AT EXISTING HOLE NDT HFEC CRACK TERMINATES AT EXISTING HOLE IAW NDTSPM06-10-01. FABRICATED REPAIR ANGLE AND DOUBLER IAW SRM 52-2-0 FIG 2 AND 51-3-0.