What was found
DURING ROUTINE C-CHECK INSP, FOUND CRACK AT STA 580 STRINGER 16R. FABRICATED AND INSTALLED REPAIR, ALODINED AND PRIMED IAW SRM 51-30-2, 51-10-2, 51-40-3, 53-10-4.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING ROUTINE C-CHECK INSP, FOUND CRACK AT STA 580 STRINGER 16R. FABRICATED AND INSTALLED REPAIR, ALODINED AND PRIMED IAW SRM 51-30-2, 51-10-2, 51-40-3, 53-10-4.