As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
BS 1661 FRAME S-18R HAS AN ELONGATED FASTENER HOLE COMMON TO THE FRAME FAIL SAFE CHORD AND STRINGER CLIP. COMPLIED WITH F-5310-162418 FUSELAGE- ELONGATED HOLE IN FRAME AND FAILSAFE CHORD AT BS 1661 AND S-18R. DUE TO THE DISCREPANCY EFFECTING THE PTF MOD A REPAIR WAS ACCOMPLISHED ON STAM EA 757-5362-16-F3816 AND STAM NR 47748980001, STA 1661 S-18R. THIS N/R IS FOR TIME TRACKING PURPOSES ONLY. MAJOR REPAIR.