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2018-03-05

final rule

Airworthiness Directives; Various Aircraft Equipped With BRP-Rotax GmbH & Co KG 912 A Series Engine

Unsafe Condition: Power loss and engine RPM drop have been reported on Rotax 912/914 engines in service. It has been determined that, due to a quality control deficiency in the manufacturing process of certain valve...

Effective: Mar 20, 2018 Category: aircraft Compliance: Within 50 flight hours

Why matched: Airworthiness Directives; Various Aircraft Equipped With BRP- Rotax GmbH & Co KG 912 A Series Engine

2016-23-06

final rule

Airworthiness Directives; Various Aircraft Equipped With BRP-Powertrain GmbH & Co KG 912 A Series Engine

Unsafe Condition: Manufacturing defect in certain carburetor floats (Part Number 861185) where a partial separation of the float outer skin may occur during engine operation, leading to separated particles that coul...

Effective: Dec 23, 2016 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Various Aircraft Equipped With BRP- Powertrain GmbH & Co KG 912 A Series Engine

2016-12-02

final rule

Airworthiness Directives; Various Aircraft Equipped With BRP-Powertrain GmbH & Co KG 912 A Series Engine

Unsafe Condition: A design change of the engine cylinder head temperature sensor without a concurrent revision of the engine model designation, engine part number, or cockpit indication to the pilot. This change sub...

Effective: Jul 15, 2016 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Various Aircraft Equipped With BRP- Powertrain GmbH & Co KG 912 A Series Engine

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

2013-17-04

final rule

Airworthiness Directives; Various Aircraft Equipped With Rotax Aircraft Engines 912 A Series Engine

Unsafe Condition: Oil leaks in the intake channel in the area of the valve guide on some cylinder heads could increase oil consumption and result in engine stoppage.

Effective: Sep 24, 2013 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Various Aircraft Equipped With Rotax Aircraft Engines 912 A Series Engine

2012-15-01

final rule

Airworthiness Directives; Various Aircraft Equipped With Rotax Aircraft Engines 912 A Series Engine

Unsafe Condition: Deviation in the manufacturing process of fuel hoses installed on the pressure side of part number 893114 fuel pumps, which may not be fuel resistant, could lead to detachment of particles from the...

Effective: Aug 14, 2012 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Various Aircraft Equipped With Rotax Aircraft Engines 912 A Series Engine

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

2012-01-01

final rule

Airworthiness Directives; Various Aircraft Equipped With Rotax Aircraft Engines 912 A Series Engine

Unsafe Condition: Deviation in the manufacturing process of certain part number 888164 crankshafts may cause cracks on the surface of the crankshaft on the power take off side, which could lead to failure of the cra...

Effective: Jan 26, 2012 Category: aircraft Compliance: Within 4 hours time-in-service

Why matched: Airworthiness Directives; Various Aircraft Equipped With Rotax Aircraft Engines 912 A Series Engine

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

2011-14-09

final rule

Airworthiness Directives; Various Aircraft Equipped With Rotax Aircraft Engines 912 A Series Engine

Unsafe Condition: Deviation in hardening of Part Number 944072 washers exceeds design specification, potentially leading to cracks in the washer, loosening of the magneto flywheel hub, and ignition failure, which co...

Effective: Jul 25, 2011 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Various Aircraft Equipped With Rotax Aircraft Engines 912 A Series Engine

2010-23-17

final rule

Airworthiness Directives; Various Aircraft Equipped With Rotax Aircraft Engines 912 A Series Engines

Unsafe Condition: Reports of cracks in the engine crankcase.

Effective: Dec 22, 2010 Category: aircraft Compliance: Before further flight.

Why matched: Airworthiness Directives; Various Aircraft Equipped With Rotax Aircraft Engines 912 A Series Engines

2010-17-08

final rule

Airworthiness Directives; Various Aircraft Equipped With Rotax Aircraft Engines 912 A Series 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: Sep 22, 2010 Category: aircraft Compliance: Within 25 hours time-in-service after September 22, 2010

Why matched: Airworthiness Directives; Various Aircraft Equipped With Rotax Aircraft Engines 912 A Series Engines

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

2009-12-14

final rule

Airworthiness Directives; Aeromot-Industria Mecanico Metalurgica ltda. Model AMT-200 and AMT-300 Series Gliders

Unsafe Condition: The coolant liquid EVANS NPG + is a flammable fluid. The engine liquid cooling system of the affected Aeromot aircrafts is not designed to operate with flammable liquids, leading to an unacceptable...

Effective: Jul 17, 2009 Category: aircraft Compliance: Within the next 20 hours time-in-service after July 17, 2009, or within the next 30 days after Ju...

Why matched: Airworthiness Directives; Aeromot-Industria Mecanico Metalurgica ltda. Model AMT-200 and AMT-300 Series Gliders

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

2007-23-15

final rule

Airworthiness Directives; Aeromot-Industria Mecanico Metalurgica Ltda. Model AMT-100/200/200S/300 Gliders

Unsafe Condition: Incorrect use of self-locking nuts in bolts subject to rotational loads in bolted fittings of some assemblies of metallic components may result in disconnection of those fittings, jeopardizing the ...

Effective: Dec 26, 2007 Category: aircraft Compliance: Within 50 hours time-in-service (TIS) after December 26, 2007

Why matched: Airworthiness Directives; Aeromot-Industria Mecanico Metalurgica Ltda. Model AMT-100/200/200S/300 Gliders

Technical illustration of an aircraft flight control surface and actuator
Problem area Flight controls

2001-23-16

final rule

Airworthiness Directives; Aeromot-Industria Mecanico Metalurgica Itda. Models AMT-100 and AMT-200 Powered Sailplanes

Unsafe Condition: Bending or warping in the main landing gear lever could interfere with the elevator control rod, potentially jamming the elevator control and leading to loss of control.

Effective: Dec 7, 2001 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Aeromot-Industria Mecanico Metalurgica Itda. Models AMT-100 and AMT-200 Powered Sailplanes

Amdt-39-10670

final rule

Airworthiness Directives; Aeromot-Industria Mecanico Metalurgica Ltda. Model AMT-200 Powered Gliders

Unsafe Condition: Inefficiency of the engine lubricating system because of ineffective flexible hoses, which could result in an in-flight engine shutdown with consequent loss of powered glider controllability.

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

98-15-19

final rule

Airworthiness Directives; Aeromot-Industria Mecanico Metalurgica Ltda. Model AMT-200 Powered Gliders

Unsafe Condition: Inefficiency of the engine lubricating system because of ineffective flexible hoses, which could result in an in-flight engine shutdown with consequent loss of powered glider controllability.

Effective: Sep 7, 1998 Category: aircraft Compliance: within the next 50 hours time-in-service (TIS) after the effective date of this AD

Why matched: Airworthiness Directives; Aeromot-Industria Mecanico Metalurgica Ltda. Model AMT-200 Powered Gliders

Amdt-39-10366

final rule

Airworthiness Directives; Aeromot-Industria Mecanico Metalurgica Ltda. Models AMT-100 and AMT-200 Powered Gliders

Unsafe Condition: Failure of the main landing gear, which could result in loss of control of the glider during landing operations.

Effective: Apr 17, 1998 Category: aircraft Compliance: Before further flight
Technical illustration of an aircraft landing gear and wheel assembly
Problem area Landing gear

98-05-05

final rule

Airworthiness Directives; Aeromot-Industria Mecanico Metalurgica Ltda. Models AMT-100 and AMT-200 Powered Gliders

Unsafe Condition: Failure of the main landing gear, which could result in loss of control of the glider during landing operations.

Effective: Apr 17, 1998 Category: aircraft Compliance: Required within the next 30 days after the effective date of this AD, unless already accomplished.

Why matched: Airworthiness Directives; Aeromot-Industria Mecanico Metalurgica Ltda. Models AMT-100 and AMT-200 Powered Gliders

Technical illustration of an aircraft landing gear and wheel assembly
Problem area Landing gear

Amdt-39-10098

final rule

Airworthiness Directives; Aeromot-Industria Mecanico Metalurgica Ltda. Model AMT-200 Powered Sailplanes

Unsafe Condition: Failure of the forward horizontal stabilizer bolt, P/N 53451, due to low cycle fatigue cracks induced by overtorquing.

Effective: Aug 15, 1997 Category: aircraft Compliance: Immediately

97-15-07

final rule

Airworthiness Directives; Aeromot-Industria Mecanico Metalurgica Ltda. Model AMT-200 Powered Sailplanes

Unsafe Condition: Failure of the forward horizontal stabilizer bolt, part number 53451, caused by a low cycle fatigue crack induced by over torquing the bolt.

Effective: Aug 15, 1997 Category: aircraft Compliance: Required as indicated after the effective date of this AD (August 15, 1997), except for those rec...

Why matched: Airworthiness Directives; Aeromot-Industria Mecanico Metalurgica Ltda. Model AMT-200 Powered Sailplanes