As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
EA 5320-02076 REV B & 2013-23-04 AMDT 39-17659 PERFORMED EA 5320-02076 REV B OP002 STEP 2 2 B. HFEC INSPECTED THE FASTENER HOLE FOUND CRACK INDICATION. L=0.005". DISASSEMBLED SEAT TRACK TO DETERMINE ACTUAL LOCATION OF CRACK IAW SRM 51-40-02 GEN REV 50. REPAIRED THE FITTING TERMINATION IAW NR CARD 53-082. ACP RII INSPECTION IAW ALL CRITICAL STEP S IN GMM 09-25-05.