What was found
(CAN) INSPECTION PER CF82-26R1 CORROSION WAS FOUND ON END FITTINGS BEYOND .040 INCH. TIE BAR REPLACED IAW WITH SB 3/37.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(CAN) INSPECTION PER CF82-26R1 CORROSION WAS FOUND ON END FITTINGS BEYOND .040 INCH. TIE BAR REPLACED IAW WITH SB 3/37.