As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NR 4 SLAT, OTBD RIB WS 198 CRACKED, 1 INCH LONG. INSTALLED REPAIR DOCUMENTED IN BOEING SRM 51-40-3. CUT OUT DAMAGED AREA OF RIB. FABRICATED DOUBLER USING .050 INCH 2024 T-3 ALUMINUM. FABRICATED ANGLE USING .063 INCH 2024 T-3 ALUMINUM. APPLIED PROTECTIVE TREATMENT IAW BSRM 51-10-2. INSTALLED DOUBLER AND ANGLE ON RIB. REBALANCING OF SLAT NOT REQUIRED. NO WEIGHT AND BALANCE CHANGE. (X)