As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RIB CRACKED LT WING IB FOREFLAP REMOVED LH IB FORE FLAP OB END RIB IAW SRM 51-30-2 AND FABRICATED NEW RIB FROM 2024O .040 HEAT TREATED TO T4 CONDITION DIM: 7" X 5 1/2" IAW ER 2-37153-801 REV A AND SRM 51-20-1 AND SRM 57-50-2 FIG 5. INSTALLED NEW RIB LT IB FOREFLAP OB END IAW SRM 51-30-2 AND EA 7-5750-143908.