As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RIGHT WING TRANSVERSE WEB UPPER O/B LEG IS CRACKED AT O/B ATTACH RIVET<[01] RIGHT WING TRANSVERSE WEB CRACK L = 0.900' AND IS FOUND OUT OF LIMITS PER SRM 57-51-02-1A-1 ALLOWABLE DAMAGE 1; PARR. 4.B.(1)(A); FIG 108.<BR>REMOVED AND REPLACED TRANSVERSE WEB IAW SRM 51-40-02-0G-0 AND DWG. 115A2512; REV.-;[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.