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2026-04-02

final rule

Airworthiness Directives; BRP-Rotax GmbH & Co KG (Formerly BRP-POWERTRAIN GMBH & CO KG and Bombardier-Rotax GmbH) Engines

Unsafe Condition: an occurrence was reported of the M40 x 1.5 collar nut that had not been installed on the propeller gearbox of a recently manufactured engine, which could result in the propeller shaft being pulled...

Effective: Mar 19, 2026 Category: propeller Compliance: Before further flight

Why matched: Airworthiness Directives; BRP-Rotax GmbH & Co KG (Formerly BRP-POWERTRAIN GMBH & CO KG and Bombardier-Rotax GmbH) Engines

Technical illustration of an aircraft propeller assembly
Problem area Propeller

2025-15-03 Recurring

final rule

Airworthiness Directives; BRP-Rotax GmbH & Co KG (Formerly BRP-POWERTRAIN GMBH & CO KG and Bombardier-Rotax GmbH) Engines

Unsafe Condition: Deviations during the manufacturing process that caused incorrect application of a certain thread-locker to certain sprag clutch housing and oil spray nozzles, which could cause blockage of the oil...

Effective: Aug 6, 2025 Category: engine Compliance: Within 50 flight hours

Why matched: Airworthiness Directives; BRP-Rotax GmbH & Co KG (Formerly BRP-POWERTRAIN GMBH & CO KG and Bombardier-Rotax GmbH) Engines

Technical illustration of an aircraft electrical generator and wiring assembly
Problem area Electrical system

2025-07-02 Recurring

final rule

Airworthiness Directives; BRP-Rotax GmbH & Co KG (Formerly BRP-POWERTRAIN GMBH & CO KG and Bombardier-Rotax GmbH) Engines

Unsafe Condition: Deviations during the manufacturing process of certain sprag clutch housing and oil spray nozzles caused incorrect application of a certain thread-locker, potentially leading to blockage of the oil...

Effective: Apr 21, 2025 Category: engine Compliance: Within 25 flight hours or within 12 months after the effective date of this AD, whichever occurs ...

Why matched: Airworthiness Directives; BRP-Rotax GmbH & Co KG (Formerly BRP-POWERTRAIN GMBH & CO KG and Bombardier-Rotax GmbH) Engines

Technical illustration of an aircraft electrical generator and wiring assembly
Problem area Electrical system

2023-17-13 Recurring

final rule

Airworthiness Directives; BRP-Rotax GmbH & Co KG (Formerly BRP-POWERTRAIN GMBH & CO KG and Bombardier-Rotax GmbH) Engines and Various Aircraft

Unsafe Condition: Surface abnormalities on the propeller shaft, caused by a deviation in the machining process, could lead to increased wear of the propeller shaft bearings, which could result in failure of the prop...

Effective: Sep 20, 2023 Category: propeller Compliance: Within 50 flight hours after the effective date of this AD.

Why matched: Airworthiness Directives; BRP-Rotax GmbH & Co KG (Formerly BRP-POWERTRAIN GMBH & CO KG and Bombardier-Rotax GmbH) Engines and Various Aircraft

Technical illustration of an aircraft propeller assembly
Problem area Propeller

2011-12-04

final rule

Airworthiness Directives; BRP-Powertrain GmbH & Co. KG Rotax 912 F3, 912 S2, 912 S3, 912 S4, 914 F2, 914 F3, and 914 F4 Reciprocating Engines

Unsafe Condition: Deviation in hardening of certain Part Number (P/N) 944072 washers exceeds the hardness of the design specification, affecting the magneto ring flywheel hub installation.

Effective: Jun 27, 2011 Category: aircraft Compliance: Within 10 flight hours or at next maintenance after the effective date of the AD, whichever occur...

Why matched: Airworthiness Directives; BRP-Powertrain GmbH & Co. KG Rotax 912 F3, 912 S2, 912 S3, 912 S4, 914 F2, 914 F3, and 914 F4 Reciprocating Engines

2010-20-23 Recurring

final rule

Airworthiness Directives; Bombardier-Rotax GmbH Type 912 F, 912 S, and 914 F Series Reciprocating Engines

Unsafe Condition: Oil loss caused by cracks in the engine crankcase, which could lead to in-flight failure of the engine and forced landing.

Effective: Nov 8, 2010 Category: engine Compliance: Within 50 hours time-in-service from the effective date

Why matched: Airworthiness Directives; Bombardier-Rotax GmbH Type 912 F, 912 S, and 914 F Series Reciprocating Engines

2010-18-14

final rule

Airworthiness Directives; Bombardier-Rotax GmbH 912 F Series and 912 S Series Reciprocating Engines

Unsafe Condition: Due to high fuel pressure, caused by exceeding pressure in front of the mechanical fuel pump (e.g., due to an electrical fuel pump), in limited cases a deviation in the fuel supply could occur. Thi...

Effective: Oct 13, 2010 Category: aircraft Compliance: Within 25 hours of engine operation after the effective date

Why matched: Airworthiness Directives; Bombardier-Rotax GmbH 912 F Series and 912 S Series Reciprocating Engines

2008-26-05

final rule

Airworthiness Directives; Bombardier-Rotax GmbH 914 F Series Reciprocating Engines

Unsafe Condition: Occurrence of cracks in the exhaust muffler in the area of the exhaust bottom and exhaust flange, which could lead to toxic contamination inside the cabin.

Effective: Jan 26, 2009 Category: aircraft Compliance: Within 12 months of the effective date (January 26, 2009).

Why matched: Airworthiness Directives; Bombardier-Rotax GmbH 914 F Series Reciprocating Engines

2005-01-14

final rule

Airworthiness Directives; Bombardier-Rotax GmbH Type 912 F, 912 S, and 914 F Series Reciprocating Engines

Unsafe Condition: The oil level in the oil tank can fall below the minimum level required to sustain proper engine lubrication, leading to inadequate venting of the lubrication system and potential damage to the eng...

Effective: Feb 15, 2005 Category: engine Compliance: Within 100 hours time-in-service (TIS) after the effective date of the AD, or at the next oil cha...

Why matched: Airworthiness Directives; Bombardier-Rotax GmbH Type 912 F, 912 S, and 914 F Series Reciprocating Engines

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

2002-21-16

final rule

Airworthiness Directives; Bombardier-Rotax GmbH Type 912 F, 912 S and 914 F Series Reciprocating Engines

Unsafe Condition: Inadequate venting of the lubrication system can lead to damage to the engine valve train, resulting in in-flight engine failure and forced landings.

Effective: Oct 28, 2002 Category: engine Compliance: Before further flight.

Why matched: Airworthiness Directives; Bombardier-Rotax GmbH Type 912 F, 912 S and 914 F Series Reciprocating Engines

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

2002-19-09 Recurring

final rule

Airworthiness Directives; Bombardier-Rotax GmbH 912 F and 912 S Series Reciprocating Engines

Unsafe Condition: Fuel leakage from the fuel pump assembly, which could result in an engine fire.

Effective: Oct 10, 2002 Category: engine Compliance: Before further flight.

Why matched: Airworthiness Directives; Bombardier-Rotax GmbH 912 F and 912 S Series Reciprocating Engines

2002-16-07

final rule

Airworthiness Directives; Bombardier-Rotax GmbH Type 912 F, 912 S, and 914 F Series Reciprocating Engines

Unsafe Condition: Reports of cracked valve spring retainers, part number 854.182, have been discovered in-service, which could lead to engine failure while in-flight.

Effective: Sep 3, 2002 Category: engine Compliance: Before further flight.

Why matched: Airworthiness Directives; Bombardier-Rotax GmbH Type 912 F, 912 S, and 914 F Series Reciprocating Engines

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

2002-10-14 Recurring

final rule

Airworthiness Directives; Bombardier-Rotax GmbH 914 F Series Reciprocating Engines

Unsafe Condition: Cracks in exhaust bend assemblies between cylinder heads and exhaust manifold assembly.

Effective: Jun 12, 2002 Category: engine Compliance: Within 50 flight hours after the effective date of the AD.

Why matched: Airworthiness Directives; Bombardier-Rotax GmbH 914 F Series Reciprocating Engines

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

Amdt-39-10667

final rule

Airworthiness Directives; Bombardier-Rotax GmbH 912 F Series Reciprocating Engines

Unsafe Condition: Fuel leaks at the outlet port of the fuel pump could result in undetected loss of fuel in flight or an engine fire.

Effective: Aug 7, 1998 Category: engine Compliance: Before further flight

Why matched: Airworthiness Directives; Bombardier-Rotax GmbH 912 F Series Reciprocating Engines

98-15-16

final rule

Airworthiness Directives; Bombardier-Rotax GmbH 912 F Series Reciprocating Engines

Unsafe Condition: Fuel leaks at the outlet port of the fuel pump due to misalignment of the rigid tube connecting the fuel distribution manifold and fuel pump, which could result in undetected loss of fuel in flight...

Effective: Aug 7, 1998 Category: engine Compliance: At the earliest of: prior to exceeding 25 hours time in service (TIS) after the effective date of...

Why matched: Airworthiness Directives; Bombardier-Rotax GmbH 912 F Series Reciprocating Engines

2002-16-26

final rule

Airworthiness Directives; Bombardier-Rotax GmbH Type 912 F and 914 F Series Reciprocating Engines; Correction

Unsafe Condition: This document makes a correction to Airworthiness Directive (AD) 2002-16-26, applicable to Bombardier-Rotax GmbH type 912 F and 914 F series reciprocating engines. AD 2002-16-26 was published in th...

Category: aircraft

Why matched: Airworthiness Directives; Bombardier-Rotax GmbH Type 912 F and 914 F Series Reciprocating Engines; Correction