As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT FRAME 16 DOUBLER JOGGLE HOLE LETTER ''A'' HAS CRACK INDICATIO N IN THE FRAME LAYER AT THE 3 OCLOCK POSITION 100% S.H. SRI 53-11-12-205-008 AT 6800 FLIGHT CYCLES SINCE REPAIR FLIGHT HOURS ARE NOT RELEVANT FOR THESE REPETITIVE INSPECTIONS. EMBODIMENT AND SUBSEQUENT INSPECTIONS AT 6800 FLIGHT CYCLES. REPAIRED HOLE A IAW SRM 53-11-12-300-012. FINAL HOLE DIAMETER AFTER ALL REWORK IS .247. REPETITIVE INSPECTIONS REQUIRED PER