As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FS 621 RPB WEB HAS 2 AREAS OF CRACK INDICATIONS NOTED IN THE Z MEMBER HEEL LINE AREA AT BL WL 126 TO WL 134 BY 60% FSH AND AT BL 0 WL110 TO WL 114 BY 70% FSH. BOTH AREAS FAILED NDT. REPLACED AND INSTALLED UPPER AND LOWER ENGINE BEAM SUPPORT ANGLES AT BL 0 IAW REO 601R-53-61-1285 REV E SHEET 17 VIEW KK.