Rolls-Royce Deutschland Ltd & Co KG Airworthiness Directives

170 ADs indexed for Rolls-Royce Deutschland Ltd & Co KG aircraft.

Models

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

final rule

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

final rule

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

final rule

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

final rule

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

View all Rolls-Royce Deutschland Ltd & Co KG ADs →