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2025-02-12 Recurring

final rule

Airworthiness Directives; Austro Engine GmbH Engines

Unsafe Condition: Reports of piston failures due to dimensional deviations in the piston pin bore and in the piston diameter, which could cause piston failure, with consequent loss of oil, loss of engine power, and ...

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

Why matched: Airworthiness Directives; Austro Engine GmbH Engines

2024-19-10 Recurring

final rule

Airworthiness Directives; Austro Engine GmbH Engines

Unsafe Condition: Reports of engine failures and cracks on the pistons with part number E4A-72-400-000.

Effective: Oct 9, 2024 Category: engine Compliance: Before further flight for engines that have reached 100 or 200 flight hours after installation, d...

Why matched: Airworthiness Directives; Austro Engine GmbH Engines

2024-05-01

final rule

Airworthiness Directives; Austro Engine GmbH Engines

Unsafe Condition: Reports of engine failures and the determination that certain batches of cap screws, installed on the inner main bearing positions of the engine, were manufactured at the lower end of the material ...

Effective: Mar 11, 2024 Category: engine Compliance: Before further flight

Why matched: Airworthiness Directives; Austro Engine GmbH Engines

2023-20-03 Recurring

final rule

Airworthiness Directives; Austro Engine GmbH Engines

Unsafe Condition: Piston failures due to dimensional deviations in the piston pin bore and piston diameter, which could lead to loss of oil, loss of engine power, and reduced control of the airplane.

Effective: Dec 11, 2023 Category: engine Compliance: Within the applicable compliance times specified in the AD, which are not detailed in the provide...

Why matched: Airworthiness Directives; Austro Engine GmbH Engines

2022-03-03

final rule

Airworthiness Directives; Austro Engine GmbH Engines

Unsafe Condition: Failure of the high pressure pump (HPP) driving gear due to a worn out assembly tool P/N AE300T012-1, and a stack up of tolerances between the cylinder head, cylinder head backside cover, camshaft ...

Effective: Feb 14, 2022 Category: engine Compliance: Before further flight

Why matched: Airworthiness Directives; Austro Engine GmbH Engines

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

2021-24-10

final rule

Airworthiness Directives; Austro Engine GmbH Engines

Unsafe Condition: prevent failure of the engine lubrication system. The unsafe condition, if not addressed, could result in failure of the engine, in-flight shutdown, and loss of the airplane.

Effective: Dec 27, 2021 Category: engine Compliance: Within the compliance times specified, unless already done.

Why matched: Airworthiness Directives; Austro Engine GmbH Engines

2021-22-20

final rule

Airworthiness Directives; Austro Engine GmbH Engines

Unsafe Condition: Failure of the high-pressure pump (HPP) driving gear due to a worn out assembly tool and a stack up of tolerances between the cylinder head, cylinder head cover, camshaft gear, and HPP gear.

Effective: Nov 16, 2021 Category: engine Compliance: Before further flight or within a certain number of flight hours after the effective date of this...

Why matched: Airworthiness Directives; Austro Engine GmbH Engines

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

2021-17-01

final rule

Airworthiness Directives; Austro Engine GmbH Engines

Unsafe Condition: An occurrence was reported of oil pressure loss on an E4 engine. Subsequent investigation determined that a certain batch of oil pumps was produced with a dimensional deviation on the inner gear/sh...

Effective: Aug 23, 2021 Category: engine Compliance: Before further flight

Why matched: Airworthiness Directives; Austro Engine GmbH Engines

2021-09-04

final rule

Airworthiness Directives; Austro Engine GmbH Engines

Unsafe Condition: Occurrences were reported of oil pump blockage on E4-A and E4-B engines. Subsequent investigation determined that the blockage was caused by oil contamination with casting sand from the production ...

Effective: May 10, 2021 Category: engine Compliance: Within 30 days, before accumulating 10 flight hours, or during the next scheduled maintenance, wh...

Why matched: Airworthiness Directives; Austro Engine GmbH Engines

2020-22-14 Recurring

final rule

Airworthiness Directives; Austro Engine GmbH Engines

Unsafe Condition: Occurrences were reported where, on some engines, turbocharger waste gate control rods were found broken and/or disconnected. Investigation results indicate that these failures were due to insuffic...

Effective: Dec 10, 2020 Category: engine Compliance: Before further flight

Why matched: Airworthiness Directives; Austro Engine GmbH Engines

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

2020-15-05

final rule

Airworthiness Directives; Austro Engine GmbH Engines

Unsafe Condition: considerable wear of the timing chain on the affected engines

Effective: Aug 31, 2020 Category: engine Compliance: Within 30 days after the effective date of this AD

Why matched: Airworthiness Directives; Austro Engine GmbH Engines

2020-14-07

final rule

Airworthiness Directives; Austro Engine GmbH Engines

Unsafe Condition: considerable wear of the timing chain and failure of fuel injectors on these engines

Effective: Aug 25, 2020 Category: engine Compliance: within 100 flight hours after the windmilling restart, or before the timing chain exceeds 900 fli...

Why matched: Airworthiness Directives; Austro Engine GmbH Engines

2018-18-02

final rule

Airworthiness Directives; Austro Engine GmbH Engines

Unsafe Condition: Considerable wear of the timing chain has been detected on some engines. This may have been caused by windmilling restarts, which are known to cause high stress to the timing chain. This condition,...

Effective: Nov 29, 2018 Category: engine Compliance: Before further flight

Why matched: Airworthiness Directives; Austro Engine GmbH Engines

2018-07-16

final rule

Airworthiness Directives; Austro Engine GmbH Engines

Unsafe Condition: Occurrences have been reported where, on some engines, turbocharger waste gate control rods were found broken and/or disconnected. Investigation results indicate that these failures were due to ins...

Effective: Apr 27, 2018 Category: engine Compliance: Within 50 flight hours or 2 months

Why matched: Airworthiness Directives; Austro Engine GmbH Engines

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

2014-08-10

final rule

Airworthiness Directives; Austro Engine GmbH Engines

Unsafe Condition: Failure of the waste gate controller lever due to fracture, leading to damage to one or more engines, loss of thrust control, and damage to the airplane.

Effective: Jun 3, 2014 Category: engine Compliance: Within 110 flight hours, the next maintenance action for any reason, or within three months after...

Why matched: Airworthiness Directives; Austro Engine GmbH Engines

2013-14-08

final rule

Airworthiness Directives; Austro Engine GmbH Engines

Unsafe Condition: Fracture of the waste gate controller lever leading to power loss events.

Effective: Aug 21, 2013 Category: engine Compliance: Within 110 flight hours, or within three months after the effective date, whichever occurs first.

Why matched: Airworthiness Directives; Austro Engine GmbH Engines

2011-18-19 Recurring

final rule

Airworthiness Directives; Austro Engine GmbH Model E4 Diesel Piston Engines

Unsafe Condition: Excessive oscillations in the fuel pressure supply can expose high-pressure (HP) fuel pumps to damaging pressure oscillations, potentially leading to engine power loss or in-flight shutdown.

Effective: Oct 6, 2011 Category: engine Compliance: Within 10 flight hours after the effective date for engines with 45 flight hours or more; before ...

Why matched: Airworthiness Directives; Austro Engine GmbH Model E4 Diesel Piston Engines

2010-23-09

final rule

Airworthiness Directives; Austro Engine GmbH Model E4 Diesel Piston Engines

Unsafe Condition: Several power loss events have been reported, due to rail pressure control failures. Analyses have shown that high pressure (HP) fuel pumps failed as a result of pressure oscillations in the fuel s...

Effective: Nov 22, 2010 Category: engine Compliance: Within 10 flight hours after the effective date of this AD for engines with 45 flight hours or mo...

Why matched: Airworthiness Directives; Austro Engine GmbH Model E4 Diesel Piston Engines