What was found
DURING ROUTINE C-CHECK INSPECTION, LONGERON 33 LEFT, SPLICE FITTING, AT STA 1694, WAS FOUND CRACKED. THE CRACK WAS .375 INCH IN LENGTH AT THE FORWARD END OF THE FITTING. THE CRACK WAS REMOVED FROM THE SPLICE FITTING AND REINSTALLED IAW DRAWING COO-SJO-96-0139DAC AND COO-SJO-96-014DAC, WHICH IS FAA DER APPROVED. (X)