What was found
CRACK ON PULLEY ATTACH ANGLE ON FORWARD SIDE OF FRAME AT BS 246, BL 0. REPLACED THE ATTACH ANGLE IAW SRM 53-10-51-2R3 AND EA 267806.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON PULLEY ATTACH ANGLE ON FORWARD SIDE OF FRAME AT BS 246, BL 0. REPLACED THE ATTACH ANGLE IAW SRM 53-10-51-2R3 AND EA 267806.