EASA AD CF-2026-44
Sep 1, 2026Engine – High Pressure Turbine – 1st and 2nd-Stage Disks Suspected Material Defect - Replacement
Canadian Airworthiness Directive CF-2026-44 addresses suspected material defects in the high pressure turbine (HPT) 1st and 2nd-stage disks of Pratt & Whitney Canada PW307A and PW307D engines. This directive mandates replacement of specific affected HPT disks to prevent uncontained disk failure that could lead to engine and aircraft damage. The directive applies to engines installed on aircraft such as the Airbus A321-231 powered by these engines.
- Pratt & Whitney Canada PW307
- Airbus A321