What was found
CRACK ON ANGLE CLIP AFT FACE, BS 400 STRINGER 26L. MEASUREMENT OF CRACK IS L: 0.530 INCHES. REPLACED THE ANGLE CLIP IAW SRM 51-40-02-0G, SRM 51-10-02-0G, PARAGRAPH 9, AND DWG 143A7505 SHEET 137, REV-.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON ANGLE CLIP AFT FACE, BS 400 STRINGER 26L. MEASUREMENT OF CRACK IS L: 0.530 INCHES. REPLACED THE ANGLE CLIP IAW SRM 51-40-02-0G, SRM 51-10-02-0G, PARAGRAPH 9, AND DWG 143A7505 SHEET 137, REV-.