As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
STA 1640 FUSELAGE FRAME WEB AND STR-14L INTERCOSTAL TEE CLIP. LOWER INBOARD HOLE HAS (2) CRACK INDICATIONS AT 3 AND 9 O`CLOCK POSITIONS. LOWER OUTBOARD HOLE HAS (1) CRACK INDICATION AT 3 TO 4 O`CLOCK POSITION. ALL WORK ACCOMPLISHED, IAW FEDEX EA F-5310-T0358129 P1 FUSEALGE-MAINFRAME-STA 1640 FRAME SPLICE REPAIR BETWEEN STRINGER I-9F AND S- 20L.