What was found
A CRACK INDICATED ON THE CONTINUITY FITTING FRAME 1, STRINGER 16. REPLACED THE CONTINUITY FITTING IAW EA 280536.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
A CRACK INDICATED ON THE CONTINUITY FITTING FRAME 1, STRINGER 16. REPLACED THE CONTINUITY FITTING IAW EA 280536.