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

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

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New ADs and bulletins for Rolls-Royce Deutschland Ltd & Co Kg TRENT 7000, summarized like the ones below, every Monday.

EASA AD 2026-0143

Jul 20, 2026

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

The document titled 'Engine – Intermediate Pressure Compressor Shaft Assembly / Front Air Seal – Inspection' is a technical directive concerning Rolls-Royce Deutschland Ltd & Co KG Trent 1000 and Trent 7000 engine models. It addresses inspection requirements for the intermediate pressure compressor shaft assembly and the front air seal components. This directive is intended to ensure the continued airworthiness and safety of affected engines installed on various aircraft.

Airworthiness Directive
  • Rolls-Royce Deutschland Ltd & Co Kg TRENT 1000
  • Rolls-Royce Deutschland Ltd & Co Kg TRENT 7000

EASA AD 2026-0141

Jul 17, 2026

Engine Oil – Lubrication / Scavenge Oil Pumps – Installation Criteria

EASA Airworthiness Directive 2026-0141 addresses installation criteria for lubrication and scavenge oil pumps on Rolls-Royce Trent 7000 series engines, which are commonly installed on Airbus A330 NEO aircraft. The directive applies to specific affected parts with certain part numbers and aims to prevent engine in-flight shutdowns caused by early-life failure of internal components in these pumps. It mandates compliance with installation criteria outlined in Rolls-Royce Alert Non-Modification Service Bulletin TRENT 1000 79-AK868.

Airworthiness Directive
  • Rolls-Royce Deutschland Ltd & Co Kg TRENT 7000
  • Airbus A330 NEO

EASA PAD 26-073

Jun 17, 2026

Engine Oil – Lubrication / Scavenge Oil Pumps – Installation Criteria

EASA Airworthiness Directive PAD No. 26-073 is a proposed directive addressing installation criteria for lubrication and scavenge oil pumps on Rolls-Royce Trent 7000 series engines, which power Airbus A330 (NEO) aircraft. The directive applies to specific part numbers of oil pumps installed on Trent 7000-68, -70, -72, -72C, and -72D engines. It aims to ensure proper installation to prevent engine failures related to low oil pressure.

Proposed AD
  • Rolls-Royce Deutschland Ltd & Co Kg TRENT 7000
  • Airbus A330

EASA AD 2025-0265

Nov 28, 2025

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.

Airworthiness Directive
  • Rolls-Royce Deutschland Ltd & Co Kg TRENT 7000

EASA AD 2025-0266

Nov 28, 2025

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.

Airworthiness Directive
  • Rolls-Royce Deutschland Ltd & Co Kg TRENT 7000

EASA AD 2025-0021R1

Jan 22, 2025

Engine – High Pressure Turbine Blades – Inspection

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.

Airworthiness DirectiveSuperseded
  • Rolls-Royce Deutschland Ltd & Co Kg TRENT 7000

EASA AD 2024-0178

Sep 12, 2024

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.

Airworthiness Directive
  • Rolls-Royce Deutschland Ltd & Co Kg TRENT 1000
  • Rolls-Royce Deutschland Ltd & Co Kg TRENT 7000
  • Boeing 787
  • Airbus A330

EASA AD 2024-0041

Feb 9, 2024

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.

AMC/GM
  • Rolls-Royce Deutschland Ltd & Co Kg TRENT 7000

EASA AD 2024-0029

Jan 29, 2024

Engine Oil — Lubrication / Scavenge Oil Pumps — Installation Criteria

The document titled 'Engine Oil — Lubrication / Scavenge Oil Pumps — Installation Criteria' issued by ROLLS-ROYCE DEUTSCHLAND Ltd & Co KG pertains to the installation requirements for lubrication and scavenge oil pumps on the Trent 7000 engine model. It provides specific criteria to ensure proper installation and functioning of these critical engine components. This document is relevant for operators and maintenance organizations working with aircraft powered by the Trent 7000 engine.

OtherSuperseded
  • Rolls-Royce Deutschland Ltd & Co Kg TRENT 7000

EASA AD 2023-0192

Nov 7, 2023

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

EASA Airworthiness Directive 2023-0192 is issued for Rolls-Royce Deutschland Trent 7000-72 and Trent 7000-72C engines. It mandates compliance with updated maintenance tasks and life limits as specified in Rolls-Royce Trent 7000 Time Limits Manual Revision 18. This directive ensures continued airworthiness by enforcing new and revised inspection and replacement requirements for critical engine components.

Airworthiness DirectiveSuperseded
  • Rolls-Royce Deutschland Ltd & Co Kg TRENT 7000

EASA AD 2023-0186

Oct 27, 2023

Air – Intermediate / High Pressure Air Tubes – Inspection

EASA Airworthiness Directive 2023-0186 addresses the inspection requirements for Rolls-Royce Trent 7000-72 and Trent 7000-72C engines, commonly installed on Airbus A330 (NEO) aircraft. This directive mandates repetitive visual inspections of intermediate pressure Stage 8 and high pressure Stage 3 air tubes to detect potential fractures that could compromise engine performance and safety. The directive applies to all serial numbers of these engine models and includes specific inspection procedures both on-wing and during shop visits.

Airworthiness DirectiveSuperseded
  • Rolls-Royce Deutschland Ltd & Co Kg TRENT 7000
  • Airbus A330

EASA AD 2022-0248

Dec 14, 2022

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

EASA Airworthiness Directive 2022-0248 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Rolls-Royce Deutschland Ltd & Co KG 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 14 dated 22 July 2022. This directive ensures continued airworthiness by requiring operators to follow the latest maintenance program amendments.

Airworthiness DirectiveSuperseded
  • Rolls-Royce Deutschland Ltd & Co Kg TRENT 7000

EASA AD 2021-0146R1

Sep 23, 2021

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.

Airworthiness Directive
  • Rolls-Royce Deutschland Ltd & Co Kg TRENT 1000
  • Rolls-Royce Deutschland Ltd & Co Kg TRENT 7000
  • Boeing 787
  • Airbus A330

EASA AD 2019-0282R1

Aug 25, 2021

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.

Airworthiness Directive
  • Rolls-Royce Deutschland Ltd & Co Kg TRENT 1000
  • Rolls-Royce Deutschland Ltd & Co Kg TRENT 7000
  • Boeing 787
  • Airbus A330

EASA AD 2020-0244

Nov 5, 2020

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

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.

Airworthiness DirectiveSuperseded
  • Rolls-Royce Deutschland Ltd & Co Kg TRENT 7000