As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FS 280 WEB CRACKED AT ALTERNATE EXTENSION PULLY BRACKET. PERFORMED ET INSPECTION IAW NDT INSPECTION PROCEDURES ET-2. ANGLE VERIFIED AS CRACKED. CUT OUT DAMAGED AREA, NDT CUTOUT AREA IAW NDTM 51-20-06. NO CRACK NOTED. REPAIRED IAW REO 601R-53-11-926.