As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
C-check/#8 axle has worn nickel plating and gouged.Corrective action/Smooth an blended out area to a .2 mm radius in ref. to repair approval sheet from Messier-Dowty OE-085-08-02-003,NDT inspected per CMM 32-09-01 section 42 no cracks found. See NDT report see page 2. Cadmium plated reworked surface IAW CMM 32-09-01.