EASA Regulations for Pratt & Whitney Canada PW210

2 airworthiness directives and regulations affecting Pratt & Whitney Canada PW210.

EASA AD CF-2026-35

Engine – Exhaust – Turbine Exhaust Frame Cracks - Inspection

The Canadian Airworthiness Directive CF-2026-35 is an urgent regulatory document addressing turbine exhaust frame (TEF) cracks in Pratt & Whitney Canada PW210A, PW210A1, and PW210S engines. It mandates initial and periodic general visual inspections of the TEF to detect circumferential cracks caused by thermal stress and material durability issues. This directive updates previous requirements to include different inspection thresholds based on TEF material composition.

Jul 16, 2026

Airworthiness DirectiveMaintenanceSafety MgmtPratt & Whitney Canada PW210

EASA AD CF-2020-13

Engine — Manual Calculation of Cycle Count for the Impeller and High Pressure Compressor Rotor

The Canadian Airworthiness Directive CF-2020-13 mandates manual calculation of cycle counts for the impeller and high pressure compressor rotor on Pratt & Whitney Canada PW210A and PW210S engines. This directive addresses inaccuracies in the Automated Damage Tracking System cycle counts to ensure these life-limited components are not operated beyond their safe limits. It applies to helicopter engines and aims to prevent potential uncontained failures that could lead to loss of control.

Apr 30, 2020

Airworthiness DirectiveMaintenanceSafety MgmtPratt & Whitney Canada PW210