Rolls-Royce plc Airworthiness Directives

565 ADs indexed for Rolls-Royce plc aircraft.

Models

Various 36 ADs Deutschland Ltd & Co KG Turbofan 25 ADs Various 8 ADs Corporation (RRC) AE 3007A Series Turbofan 5 ADs Deutschland (RRD) (Formerly Rolls-Royce, plc) TAY 611-8, TAY 620-15, TAY 650-15, and TAY 651-54 Series Turbofan 4 ADs Deutschland Ltd & Co KG 4 ADs Deutschland Ltd & Co KG (RRD) Dart 528, 529, 532, 535, 542, and 552 Series Turboprop 4 ADs plc (RR) Turbofan 4 ADs 3007A 3 ADs Deutschland (RRD) (Formerly Rolls-Royce, plc) Tay 611-8, Tay 620-15, Tay 620-15/20, Tay 650-15, Tay 650-15/10, and Tay 651-54 Turbofan 3 ADs (1971) Limited, Bristol Engine Division Model Viper Mk.601-22 Turbojet 2 ADs 611-8 620-15 650-15 651-54 2 ADs Corporation (Formerly Allison Engine Company) 250-B17B, -B17C, -B17D, -B17E, -C20, -C20B, -C20F, -C20J, -C20S, and -C20W Turboprop and Turboshaft 2 ADs Corporation (Formerly Allison Engine Company) 250-C20 Series Turboshaft and 250-B17 Series Turboprop 2 ADs Corporation (Formerly Allison Engine Company) AE 3007 Series Turbofan 2 ADs Deutschland (Formerly Rolls-Royce plc) Models Tay 650-15 and 651-54 Turbofan 2 ADs Deutschland Ltd & Co. KG Turbofan 2 ADs RB211-Trent 800 2 ADs plc (RR) RB211-535E4 Series Turbofan 2 ADs plc (RR) RB211-Trent 800 Series Turbofan 2 ADs 650-15 651-54 2 ADs plc RB211 Trent 768-60, 772-60, and 772B-60 Turbofan 2 ADs plc RB211 Trent 800 Series Turbofan 2 ADs Various 1 AD 401 1 AD 401A 1 AD 401B 1 AD 402 1 AD 402A 1 AD 402B 1 AD 414 1 AD N22B 1 AD N24A 1 AD Power turbine and Governor Assemblies 1 AD 3007 1 AD 501-D 1 AD 528 529 532 535 542 555 1 AD 611-8 620-15 620-15/20 650-15 650-15/10 651-54 1 AD 650-15 651-54 1 AD Corporation (Formerly Allison Engine Company) 250-C28 Series 1 AD Corporation (Formerly Allison Engine Company) 501-D Series Turboprop 1 AD Corporation (Formerly Allison Engine Company) 501-D22A, 501-D22C, and 501-D22G Turboprop 1 AD Corporation (Formerly Allison Engine Company) AE 2100 Turboprop and AE 3007 Turbofan Series 1 AD Corporation (Formerly Allison Engine Company) AE 3007A1, AE 3007A1/1, AE 3007A1/3, AE 3007A3, AE 3007A1E, and AE 3007A1P Turbofan 1 AD Corporation (Formerly Allison Engine Company) Model AE 3007A and AE 3007C Turbofan 1 AD Deutschland Ltd & Co KG (RRD) Turbofan 1 AD Deutschland Ltd & Co KG (formerly Rolls-Royce plc) Dart 528, 529, 532, 535, 542, and 552 Series Turboprop 1 AD Deutschland Ltd & Co KG Dart 528, 529, 529D, 531, 532, 535, 542, and 552 Series Turboprop 1 AD Deutschland Ltd & Co KG Dart 528, 529, 532, 535, 542, and 555 Series Turboprop 1 AD Deutschland Ltd & Co KG TAY 650-15 and TAY 651-54 Turbofan 1 AD Deutschland Ltd & Co KG Tay 611-8, Tay 611-8C, Tay 620-15, Tay 650-15, and Tay 651-54 Turbofan 1 AD Deutschland Ltd & Co KG Tay 611-8, Tay 620-15, Tay 650-15, and Tay 651-54 Series Turbofan 1 AD Deutschland Ltd & Co KG Tay 620-15 1 AD Deutschland Ltd & Co KG Tay 650-15 and Tay 651-54 Turbofan 1 AD Deutschland Ltd & Co KG Turbojet 1 AD plc (RR) RB211 Trent 500 Series Turbofan 1 AD plc (RR) RB211-22B, RB211-524, and RB211-535 Series Turbofan 1 AD plc (RR) RB211-524 Series Turbofan 1 AD plc (RR) RB211-Trent 768-60 and Trent 772-60 Turbofan 1 AD Various 1 AD Trent 1000-A2 1 AD Trent 1000-AE2 1 AD Trent 1000-C2 1 AD Trent 1000-CE2 1 AD Trent 1000-D2 1 AD Trent 1000-E2 1 AD Trent 1000-G2 1 AD Trent 1000-H2 1 AD Trent 1000-J2 1 AD Trent 1000-K2 1 AD Trent 1000-L2 1 AD Various 1 AD RB211-524G2-19 1 AD RB211-535E4-37 1 AD RB211-535E4-B-37 1 AD RB211-535E4-C-37 1 AD RB211-Trent 970-84 and RB211-Trent 972-84 engines 1 AD Deutschland Ltd. & Co. KG (Formerly Rolls-Royce plc) Turbofan 1 AD RB211 1 AD RB211 700 1 AD RB211 768 772 1 AD RB211 768-60 772-60 772B-60 1 AD RB211 800 1 AD plc Models Tay 650-15 and 651-54 Turbofan 1 AD plc. Models Tay 650-15 and 651-54 Turbofan 1 AD

Recent ADs

2026-13-06 Recurring

final rule

Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG Engines

Unsafe Condition: The main fuel hose assembly of the fuel manifold may exhibit softness, non-compliance, resistance, shrinkage, cracks, chafing, dents, kinks, necking, and degradation of the hose braid wire.

Effective: Jul 17, 2026 Category: engine

Why matched: Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG Engines

2026-10-21 Recurring

final rule

Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG Engines

Unsafe Condition: Cracking, damage, or air leakage wear in the intermediate-pressure stage 8 (IP8) and high-pressure stage 3 (HP3) air transfer tubes and front bearing housing IP8 air feed tubes.

Effective: Jul 9, 2026 Category: aircraft

Why matched: Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG Engines

2026-12-06 Recurring

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Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG Engines

Unsafe Condition: Axial cracks in the high-pressure turbine (HPT) blades could result in uncontained engine failure.

Effective: Jun 30, 2026 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG Engines

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

2026-10-06 Recurring

final rule

Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG

Unsafe Condition: Failure of the high-pressure turbine (HPT) blades could result in uncontained engine failure.

Effective: Jun 12, 2026 Category: engine Compliance: before exceeding specified flight cycles since new
Technical illustration of an aircraft turbine engine assembly
Problem area Engine

2026-04-13 Recurring

final rule

Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG Engines

Unsafe Condition: Fracture of the IP8 and HP3 air tubes could remain undetected for longer than assumed, leading to reduced efficiency of internal cooling and sealing flows, failure of the air tubes, damage to the e...

Effective: Apr 10, 2026 Category: aircraft Compliance: Within 30 days after the effective date of the AD.

Why matched: Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG Engines

2025-26-03 Recurring

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Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG Engines

Unsafe Condition: The manufacturer identified a possibility of release of an HPC mini-disc anti-rotation block into the HPC assembly stage 5 and 6 discs and at the HPC rear drum during an engine operation.

Effective: Jan 27, 2026 Category: engine Compliance: Before further flight

Why matched: Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG Engines

2025-23-10

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Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG Engines

Unsafe Condition: certain low-pressure compressor (LPC) fan blades are at risk of cracking due to incorrect dressing, which may have been performed on areas of low wall thickness and high localized internal stress l...

Effective: Dec 8, 2025 Category: aircraft Compliance: Within 30 days for most engines.

Why matched: Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG Engines

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

2025-06-03 Recurring

final rule

Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG Engines

Unsafe Condition: cracks on certain low-pressure compressor (LPC) rotor (fan) disks

Effective: Apr 23, 2025 Category: engine Compliance: Within 50 flight hours

Why matched: Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG Engines

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

2025-05-03

final rule

Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG Engines

Unsafe Condition: Failure of critical rotating parts, which, if not addressed, could result in failure of one or more engines, loss of thrust control, and loss of the airplane.

Effective: Apr 17, 2025 Category: engine Compliance: Within the compliance times specified in EASA AD 2024-0041

Why matched: Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG Engines

2025-02-14 Recurring

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Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG Engines

Unsafe Condition: Reports of cracked intermediate pressure compressor (IPC) shaft assembly front air seals. Such cracking could lead to IPC stage 1 disk burst with consequent release of high energy debris and damage...

Effective: Apr 1, 2025 Category: aircraft Compliance: Within 50 flight hours

Why matched: Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG Engines

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

2025-05-04 Recurring

final rule

Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG Engines

Unsafe Condition: Cracks found in the transition duct area of the drains mast, which is part of the fire wall in Zone 1, could result in failure of the drains mast, possible engine fire, and damage to the airplane.

Effective: Apr 1, 2025 Category: aircraft Compliance: Within 23 months of the effective date of April 1, 2025.

Why matched: Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG Engines

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

2024-25-10

final rule

Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG Engines

Unsafe Condition: Damage to a fuel manifold flexible tube was reported, which led to a controlled, temporary engine fire and heat damage to the exterior and interior of the engine nacelle (thrust reverser C-ducts). ...

Effective: Feb 18, 2025 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG Engines

2024-21-03

final rule

Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG

Unsafe Condition: Failure of critical rotating parts, which could result in failure of one or more engines, loss of thrust control, and loss of the airplane.

Effective: Jan 6, 2025 Category: engine Compliance: Within 30 days after the effective date of this AD (January 6, 2025).

Why matched: Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG

2024-23-04

final rule

Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG Engines

Unsafe Condition: Failure of critical rotating parts, which could result in failure of one or more engines, loss of thrust control, and loss of the airplane.

Effective: Jan 6, 2025 Category: aircraft Compliance: Within 30 days after the effective date of this AD.

Why matched: Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG Engines

2024-20-08

final rule

Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG Engines

Unsafe Condition: The manufacturer revised the existing engine time limits manual (TLM) to introduce new or more restrictive instructions and associated thresholds and intervals for life-limited parts, which could l...

Effective: Nov 8, 2024 Category: engine Compliance: Within 30 days after the effective date of this AD.

Why matched: Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG Engines

2024-10-14 Recurring

final rule

Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG

Unsafe Condition: Cracking and separation of certain low-pressure turbine (LPT) stage 1 blade assemblies.

Effective: Aug 13, 2024 Category: aircraft Compliance: Within 50 flight hours after the effective date.

Why matched: Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

2024-10-06

final rule

Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG Engines

Unsafe Condition: unsafe condition on these products.

Effective: Jun 27, 2024 Category: engine Compliance: Within 12 months of effective date

Why matched: Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG Engines

2024-08-06

final rule

Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG

Unsafe Condition: Reports of wear in the combining spill valve (CSV) assembly of certain hydro-mechanical units (HMUs) have been reported, which can reduce the fuel flow output when the engine is operated at high po...

Effective: Jun 10, 2024 Category: aircraft Compliance: Within 4 months after the effective date of this AD.

Why matched: Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG

2024-05-12

final rule

Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG

Unsafe Condition: reports of wear in the combining spill-valve assembly of certain hydro-mechanical units

Effective: May 22, 2024 Category: aircraft Compliance: Within 50 flight hours

Why matched: Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG

2024-06-06

final rule

Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG Engines

Unsafe Condition: Failure of critical rotating parts, which could result in failure of one or more engines, loss of thrust control, and loss of the airplane.

Effective: May 21, 2024 Category: engine Compliance: Within the compliance time specified in the applicable time limits manual (TLM) for each affected...

Why matched: Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG Engines

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