As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE:C2 NR 1 ALT THRU 560A BETWEEN XRS 428 AND XRS 463 STRINGER TO FRONT SPAR FITTING CRACKED. REPLACED NR 1 ALT FRONT SPAR FITTING BETWEEN XRS 428 AND XRS 463 IAW DWG 3644046, SRM 51-03-02, SRM 51-01-08, SRM 51-01-20D AND SRM 51- 01-12.