As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED ON THE AFT TAIL COMPARTMENT RT CIRCUMFERENTIAL FRAME, AFT AND ABOVE ACCESS PANEL 62 ZONE 37. REPAIR ACCOMPLISHED, FABRICATION AND INSTALLATION OF REPAIR DOUBLER IN ACCORDANCE WITH THE DOUGLAS STRUCTURAL REPAIR MANUAL