What was found
#2 ENGINE RTF STRUT #1 HAS .500 CRACK AT LOCATION C2 FWD SIDE OF WELD AT CENTER OF CUTOUT / [01] ENGINEERING ADDED EA# M-21-172-00811; REFERENCE BARCODE# TTG8Q00E05YP.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
#2 ENGINE RTF STRUT #1 HAS .500 CRACK AT LOCATION C2 FWD SIDE OF WELD AT CENTER OF CUTOUT / [01] ENGINEERING ADDED EA# M-21-172-00811; REFERENCE BARCODE# TTG8Q00E05YP.