As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
MCN - MAJOR REPAIR - DURING C-21 CHECK A 1.125 INCH CRACK WAS FOUND IN RADIUS OF FUSELAGE FRAME CHORD, AFT OF L-1 DOOR BS 344, STR 15 LT. MAINTENANCE REMOVED DAMAGED FUSELAGE FRAME CHORD AFT OF L-1 DOOR BS 344, STR 15 LT; FABRICATED A NEW REPLACEMENT FUSELAGE FRAME CHORD; INSTALLED REPAIR PART IAW B737-200 SRM 51-30-02 FIG 7 & 11 PG 1.