EASA 2018-0268

Requires repetitive recalculation of the service life (consumed and remaining) of each affected life-limited part and replacement of each affected part before exceeding the life limit. Affected parts include low-pressure compressor (LPC) disks; LPC fan blades; fan shafts; low-pressure turbine (LPT) stage 1 disks; LPT stage 2 disks; LPT rotor shaft and annulus fillers; high-pressure compressor (HPC) stage 1 to 6 rotor disks; HPC stage 7 to 10 rotor disks and curvic rings; and high-pressure turbine (HPT) stage 1 and 2 disks.