What was found
WHILE PERFORMING REPAIR TO THE ENGINE SUPPORT BEAM PER REO 53-61-345 A CRACK WAS NOTED ON THE UNDER LAYING EXTRUDED ANGLE P/N 601-35006-7 CRACK APPROX 5/16".THE CRACK WAS REPAIRED I/A/W CANADAIR REO 601R-53-61-394.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
WHILE PERFORMING REPAIR TO THE ENGINE SUPPORT BEAM PER REO 53-61-345 A CRACK WAS NOTED ON THE UNDER LAYING EXTRUDED ANGLE P/N 601-35006-7 CRACK APPROX 5/16".THE CRACK WAS REPAIRED I/A/W CANADAIR REO 601R-53-61-394.