EASA Regulations for Rolls-Royce Deutschland Ltd & Co Kg Tay

2 airworthiness directives and regulatory documents affecting Rolls-Royce Deutschland Ltd & Co Kg Tay.

EASA AD 2024-0085

Engine — High Pressure Turbine Rotor Shaft / Spring-Loaded Pin Assembly — Inspection

The document titled 'Engine — High Pressure Turbine Rotor Shaft / Spring-Loaded Pin Assembly — Inspection' is a regulatory directive concerning the inspection of the high pressure turbine rotor shaft and spring-loaded pin assembly on Rolls-Royce Deutschland Ltd & Co KG Tay engines. It addresses specific maintenance requirements to ensure the continued airworthiness of engines equipped on aircraft using the Tay engine model.

Apr 12, 2024

Airworthiness DirectiveMaintenanceSafety MgmtRolls-Royce Deutschland Ltd & Co Kg Tay

EASA AD 2022-0184

Engine — High Pressure Turbine Stage 2 Intermediate Air Seal / Bolts — Inspection

EASA Airworthiness Directive 2022-0184 is an airworthiness directive addressing Rolls-Royce Tay 620-15 and Tay 650-15 engines, commonly installed on Fokker F28 Mark 0070 and Mark 0100 series aircraft. The directive mandates inspections of the high pressure turbine stage 2 intermediate air seal and its attachment bolts to detect cracks and prevent potential uncontained engine failures. It applies to all serial numbers of the affected engines.

Sep 2, 2022

Airworthiness DirectiveMaintenanceSafety MgmtRolls-Royce Deutschland Ltd & Co Kg TayFokker F28