What was found
DURING C-16 CHECK 2 EACH CRACKS WERE FOUND ON ATTACH ANGLES AFT OF BS 348.20, LT SIDE OF FUSELAGE, WL 222. MAINTENANCE REMOVED CRACKED ATTACH ANGLE BS 348.20, WL 222; FABRICATED 2 EACH NEW REPLACEMENT ATTACH ANGLES IAW DWG'S 69-16970-501 AND 69-76555-3; INSTALLED REPAIR PARTS IAW B737-200 SRM 51-30-02, PG. 39, FIG. 11.