As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING ROUTINE C-CHECK, FOUND A CRACK IN THE FORWARD UPPER HOLE IN THE UPPER VERTICAL FLANGE OF THE WING TO BODY RIB FITTING UPPER CHORD AT RIGHT BS 760.95. COMPLIED WITH BOEING 727 SB 727-57-0112 REV 5. INSTALLED SUPPORT ANGLE IAW BOEING 727 SB 57-0112 AND BOEING DRAWING NR 65-65492 REV B AND B727 SRM 51-30-2. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)