As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NR 5 LEADING EDGE SLAT INBOARD RIB, AT ACUATOR ATTACHMENT WS 234 IS CRACKED. REPAIRED IAW BOEING SRM 57-50-3, FIGURE 9. FABRICATED DOUBLER FROM .050 INCH 2024-T3 ALUMINUM. APPLIED PROTECTIVE TREATMENT TO ALL PARTS AS REQUIRED. INSTALLED DOUBLER. REBALANCE OF SLAT NOT REQUIRED. NO WEIGHT AND BALANCE CHANGE.