What was found
DURING VISUAL INSPECTION OF NR 2 STRUT DIAGONAL BRACE, A CRACK OF .75 INCH LONG FOUND AT FORWARD LUG TOP SURFACE. IT IS BELIEVED THE CRACK IS DUE TO FATIGUE.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING VISUAL INSPECTION OF NR 2 STRUT DIAGONAL BRACE, A CRACK OF .75 INCH LONG FOUND AT FORWARD LUG TOP SURFACE. IT IS BELIEVED THE CRACK IS DUE TO FATIGUE.