What was found
A CRACK INDICATION WAS FOUND ON CONTINUITY FITTING, REPLACED THE ANGLE IAW SRM A319 51-72-11, AND DRAWING R53112919.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
A CRACK INDICATION WAS FOUND ON CONTINUITY FITTING, REPLACED THE ANGLE IAW SRM A319 51-72-11, AND DRAWING R53112919.