As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
BS 520 LT, FOUND CRACK IN FUSELAGE FRAME FLANGE BETWEEN STR 9 AND STR 11. ALSO, SHEAR DOUBLER CRACKED IN CUT-OUT TO NEAREST FASTENER HOLE DURING SECTION 41 INSPECTION. REPAIRED STR 9 PER SRM 53-10-04, FIG 85. REPAIRED FRAME AT STR 10 PER ACC KLM DFX 99-126 REV 1. SHEAR DOUBLER AT STR 11 REPAIRED PER ACC KLM DFX 99-123. FORM 8110-3 ISSUED. (X)