What was found
PULLEY ATTACH ANGLE, STIFFENER, IS CRACKED FWD SIDE OF FRAME 246 AT LBL 7. R & R STIFFENER IAW SRM 53-10-51-2R, 51-20-05, 51-40-02 & AMM 51-20-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
PULLEY ATTACH ANGLE, STIFFENER, IS CRACKED FWD SIDE OF FRAME 246 AT LBL 7. R & R STIFFENER IAW SRM 53-10-51-2R, 51-20-05, 51-40-02 & AMM 51-20-01.