RegNotify

EASA Regulations for Rolls-Royce Deutschland Ltd & Co Kg TRENT 7000

9 airworthiness directives and regulations affecting Rolls-Royce Deutschland Ltd & Co Kg TRENT 7000.

EASA AD 2025-0265

Air — Intermediate / High Pressure Air Tubes — Inspection

EASA Airworthiness Directive 2025-0265 is an airworthiness directive addressing inspection requirements for intermediate and high pressure air tubes on Rolls-Royce Trent 7000-72 and Trent 7000-72C engines, commonly installed on Airbus A330 (NEO) aircraft. The directive mandates repetitive on-wing and in-shop visual inspections of specific air transfer and air feed tubes to ensure their structural integrity and prevent potential engine damage.

Nov 28, 2025
Airworthiness DirectiveMaintenanceSafety MgmtRolls-Royce Deutschland Ltd & Co Kg TRENT 7000

EASA AD 2025-0266

Engine — High Pressure Turbine Blades — Inspection

EASA Airworthiness Directive 2025-0266 is an airworthiness directive addressing inspection requirements for high pressure turbine (HPT) blades, part number KH64485, installed on Rolls-Royce Trent 7000-72 and Trent 7000-72C engines, commonly found on Airbus A330 (NEO) aircraft. The directive mandates on-wing borescope inspections to detect axial cracking and specifies corrective actions including engine removal and blade replacement if cracks exceed defined limits. It applies to engines except those modified with mod 72-K336, which introduces redesigned blades not affected by this unsafe condition.

Nov 28, 2025
Airworthiness DirectiveMaintenanceSafety MgmtRolls-Royce Deutschland Ltd & Co Kg TRENT 7000

EASA AD 2025-0021R1

SUPERSEDED BY EASA AD 2025-0266

EASA Airworthiness Directive 2025-0021R1 is an updated directive addressing the inspection and maintenance of Rolls-Royce Trent 7000-72 and Trent 7000-72C engines, primarily installed on Airbus A330 (NEO) aircraft. It mandates on-wing borescope inspections of high pressure turbine (HPT) blades with part number KH64485 to detect axial cracking and requires corrective actions including engine removal and blade replacement if cracks exceed specified limits. The directive also introduces a life limit for affected HPT blades and excludes engines modified with mod 72-K336 from these requirements.

Jan 22, 2025
Airworthiness DirectiveMaintenanceSafety MgmtRolls-Royce Deutschland Ltd & Co Kg TRENT 7000

EASA AD 2024-0178

Engine — Intermediate Pressure Compressor Shaft Assembly / Front Air Seal — Inspection

EASA Airworthiness Directive 2024-0178 is an airworthiness directive addressing the inspection of the intermediate pressure compressor (IPC) shaft assembly front air seal on Rolls-Royce Trent 1000 and Trent 7000 engines. These engines are commonly installed on Boeing 787 and Airbus A330 aircraft. The directive mandates repetitive inspections to detect cracks that could lead to engine failure and potential safety risks.

Sep 12, 2024
Airworthiness DirectiveMaintenanceSafety MgmtRolls-Royce Deutschland Ltd & Co Kg TRENT 1000Rolls-Royce Deutschland Ltd & Co Kg TRENT 7000Boeing 787Airbus A330

EASA AD 2024-0041

Time Limits / Maintenance Checks — Time Limits Manual / Maintenance Programme — Amendment

The document titled 'Time Limits / Maintenance Checks — Time Limits Manual / Maintenance Programme — Amendment' pertains to the Rolls-Royce Deutschland Ltd & Co KG Trent 7000 engine. It provides updated guidance and requirements related to the maintenance time limits and checks for this specific engine model. The amendment aims to ensure continued airworthiness and reliability of the Trent 7000 engine through revised maintenance protocols.

Feb 9, 2024
AMC/GMMaintenanceRolls-Royce Deutschland Ltd & Co Kg TRENT 7000

EASA AD 2021-0146R1

Time Limits / Maintenance Checks — High Pressure Turbine Disc — Inspection

EASA Airworthiness Directive 2021-0146R1 is a regulatory document addressing inspection requirements for high-pressure turbine (HPT) discs installed on Rolls-Royce Trent 1000 and Trent 7000 engines, commonly found on Boeing 787 and Airbus A330 (NEO) aircraft. The directive mandates a one-time inspection of affected HPT discs during the next qualified engine shop visit to ensure they are disassembled to piece-part level and inspected according to the applicable Rolls-Royce Time Limits Manual (TLM) tasks. This AD aims to prevent potential HPT disc failures that could lead to high-energy debris release and consequent aircraft damage.

Sep 23, 2021
Airworthiness DirectiveMaintenanceSafety MgmtRolls-Royce Deutschland Ltd & Co Kg TRENT 1000Rolls-Royce Deutschland Ltd & Co Kg TRENT 7000Boeing 787Airbus A330

EASA AD 2019-0282R1

Engine — Intermediate Pressure Compressor Shaft Assembly — Inspection

EASA Airworthiness Directive 2019-0282R1 is a regulatory document addressing inspection requirements for the intermediate pressure compressor (IPC) shaft assembly, part number KH18436, installed on Rolls-Royce Trent 1000 and Trent 7000 engines. These engines are commonly found on Boeing 787 and Airbus A330 aircraft. The directive mandates repetitive inspections to detect cracks in the IPC shaft assembly's front air seal to prevent potential engine failure.

Aug 25, 2021
Airworthiness DirectiveMaintenanceSafety MgmtRolls-Royce Deutschland Ltd & Co Kg TRENT 1000Rolls-Royce Deutschland Ltd & Co Kg TRENT 7000Boeing 787Airbus A330

EASA AD 2020-0244

SUPERSEDED BY EASA AD 2022-0248

EASA Airworthiness Directive 2020-0244 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Rolls-Royce Deutschland Trent 7000-72 and Trent 7000-72C engines. It mandates compliance with updated maintenance tasks and life limits as specified in the Rolls-Royce Trent 7000 Time Limits Manual Revision 7 dated 10 July 2020. This directive ensures continued airworthiness by requiring operators to follow the revised maintenance program and replace critical parts within updated life limits.

Nov 5, 2020
Airworthiness DirectiveMaintenanceSafety MgmtRolls-Royce Deutschland Ltd & Co Kg TRENT 7000