What was found
BS 1140, TENSION TIE AREA, FOUND CRACK AT FWD CHANNEL THROUGH THICKNESS. REPAIRED IAW SRM 53-40-30, REPAIR 2, FIG 201.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
BS 1140, TENSION TIE AREA, FOUND CRACK AT FWD CHANNEL THROUGH THICKNESS. REPAIRED IAW SRM 53-40-30, REPAIR 2, FIG 201.