As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
STRINGER CLIP 3L IS CRACKED AT BS 706<[01] VERIFY END OF CRACK AT STRINGER CLIP BS 706; S-3L;[02] ACCOMPLISHED HFEC SURFACE SCAN IAW 737 NDTM PART 6 CHAPTER 51-00-00 PROCEDURE 23. NO CRACKS NOTED.<BR><BR>EQUIPMENT USED: NORTEC 600 ID: ATS1465 CAL DUE: 09/2023;[03] HFEC INSPECTED STRINGER CLIP AT BS 706; S-3L. NO CRACK NOTED AT THIS LOCATION. NO FURTHER ACTION REQUIRED;[04] PART REQUIRED NOT USED;[05] VERIFIED CORRECTIVE ACTION 3 AND 4<BR><BR>VERIFIED MEASUREMENT TABLE