brp--powertrain gmbh & co kg Airworthiness Directives

12 ADs indexed for brp--powertrain gmbh & co kg aircraft.

Recent ADs

2016-13-04

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Airworthiness Directives; BRP-Powertrain GmbH & Co KG Reciprocating Engines

Unsafe Condition: A design change relocated the engine cylinder head temperature sensor to a new location and converted it to a coolant temperature sensor, which could result in exceeding coolant temperature limits,...

Effective: Jul 27, 2016 Category: aircraft Compliance: Within 6 months after the effective date of the AD

Why matched: Airworthiness Directives; BRP-Powertrain GmbH & Co KG Reciprocating Engines

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

2013-15-19

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Airworthiness Directives; BRP-Powertrain GmbH & Co KG Rotax Reciprocating Engines

Unsafe Condition: Cylinder heads not manufactured to proper specification may lead to excessive oil consumption, which could result in an in-flight engine shutdown, forced landing, and damage to the airplane.

Effective: Aug 27, 2013 Category: engine Compliance: Before further flight

Why matched: Airworthiness Directives; BRP-Powertrain GmbH & Co KG Rotax Reciprocating Engines

2012-16-13

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Airworthiness Directives; BRP-Powertrain GmbH & Co KG Rotax Reciprocating Engines

Unsafe Condition: Failure of the pressure side fuel hose on certain fuel pumps and contamination in the carburetors connected to those fuel pumps.

Effective: Nov 6, 2012 Category: aircraft Compliance: Within 5 flight hours after the effective date of the AD.

Why matched: Airworthiness Directives; BRP-Powertrain GmbH & Co KG Rotax Reciprocating Engines

Technical illustration of an aircraft fuel pump, filter, valve, and lines
Problem area Fuel system

2012-04-03

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Airworthiness Directives; BRP-Powertrain GmbH & Co KG Rotax Reciprocating Engines

Unsafe Condition: During engine production, some engines may not have had the oil pump attachment bolts torqued to specification, which could lead to oil leaks and irregularities in the oil supply.

Effective: Mar 16, 2012 Category: engine Compliance: Within four flight hours or 30 days after the effective date of this AD, whichever occurs first.

Why matched: Airworthiness Directives; BRP-Powertrain GmbH & Co KG Rotax Reciprocating Engines

2012-01-07

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Airworthiness Directives; BRP-POWERTRAIN GMBH & CO KG Rotax Reciprocating Engines

Unsafe Condition: Isolated manufacturing deviations reportedly found on the threads of a certain batch of fuel pressure regulators, part number (P/N) 887130, installed on Rotax 914 F series engines, which could resu...

Effective: Feb 27, 2012 Category: engine Compliance: Within 100 flight hours after the effective date of this AD

Why matched: Airworthiness Directives; BRP--POWERTRAIN GMBH & CO KG Rotax Reciprocating Engines

2011-25-02

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Airworthiness Directives; BRP-Powertrain GmbH & Co. KG Reciprocating Engines

Unsafe Condition: A deviation in the manufacturing process of certain part number (P/N) 888164 crankshafts may have resulted in a latent defect, leading to crack formation on the power takeoff side of the crankshaft...

Effective: Dec 22, 2011 Category: aircraft Compliance: Within 4 operating hours

Why matched: Airworthiness Directives; BRP-Powertrain GmbH & Co. KG Reciprocating Engines

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

2008-26-05

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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

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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

2002-19-09 Recurring

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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

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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

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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

98-15-16

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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

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