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2022-10-02 Recurring

final rule

Airworthiness Directives; Honeywell International, Inc. (Type Certificate Previously Held by AlliedSignal, Inc. and Textron Lycoming) Turboshaft Engines

Unsafe Condition: tachometer drive spur gear failure, resulting in potential engine overspeed, loss of power turbine speed (N2) instrument panel indication, and hard landings.

Effective: Jun 28, 2022 Category: engine Compliance: Within 50 flight hours

Why matched: Airworthiness Directives; Honeywell International, Inc. (Type Certificate Previously Held by AlliedSignal, Inc. and Textron Lycoming) Turboshaft Engines

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

2016-07-02

final rule

Airworthiness Directives; Honeywell International Inc. (Type Certificate Previously Held by AlliedSignal Inc., Garrett Turbine Engine Company) Turbofan Engines

Unsafe Condition: Certain interstage turbine transition (ITT) ducts failing to meet containment capability requirements.

Effective: May 5, 2016 Category: engine Compliance: Within 2,600 hours time-in-service after the effective date of this AD.

Why matched: Airworthiness Directives; Honeywell International Inc. (Type Certificate Previously Held by AlliedSignal Inc., Garrett Turbine Engine Company) Turbofan Engines

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

2014-12-52

final rule

Airworthiness Directives; Honeywell International Inc. (Type Certificate Previously Held by AlliedSignal Inc., Garrett Turbine Engine Company) Turbofan Engines

Unsafe Condition: Reports of LPT2 blade separations indicate the presence of casting anomalies at or near the root of the LPT2 blade, which could result in LPT2 blade failure, multiple engine in-flight shutdowns, an...

Effective: Jul 28, 2014 Category: engine Compliance: Before further flight

Why matched: Airworthiness Directives; Honeywell International Inc. (Type Certificate Previously Held by AlliedSignal Inc., Garrett Turbine Engine Company) Turbofan Engines

06-63

final rule

Airworthiness Directives; Honeywell International Inc. (Formerly AlliedSignal, Inc., Formerly Textron Lycoming, Formerly Avco Lycoming) T5309, T5311, T5313B, T5317A, T5317A-1, and T5317B Series, and T53-L-9, T53-L-11, T53-L-13B, T53-L-13BA, T53-L-13B S/SA, T53-L-13B S/SB, T53-L-13B/D, and T53-L-703 Series Turboshaft Engines

Unsafe Condition: Failure of certain compressor, gas producer, and power turbine rotating components, which could result in failure of the engine and possible damage to the helicopter.

Effective: Feb 16, 2006 Category: engine Compliance: Within the specified reduced life limits for affected components.

Why matched: Airworthiness Directives; Honeywell International Inc. (Formerly AlliedSignal, Inc., Formerly Textron Lycoming, Formerly Avco Lycoming) T5309, T5311, T5313B, T5317A, T5317A-1, and T5317B Series, and T53-L-9, T53-L-11, T53-L-13B, T53-L-13BA, T53-L-13B S/SA, T53-L-13B S/SB, T53-L-13B/D, and T53-L-703 Series Turboshaft Engines

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

2006-01-05

final rule

Airworthiness Directives; Honeywell International Inc. (Formerly AlliedSignal, Inc., Formerly Textron Lycoming, Formerly Avco Lycoming) T5309, T5311, T5313B, T5317A, T5317A-1, and T5317B Series, and T53-L-9, T53-L-11, T53-L-13B, T53-L-13BA, T53-L-13B S/SA, T53-L-13B S/SB, T53-L- 13B/D, and T53-L-703 Series Turboshaft Engines

Unsafe Condition: Failure of certain compressor, gas producer, and power turbine rotating components due to lower calculated service life limits than previously published.

Effective: Feb 16, 2006 Category: engine Compliance: before further flight

Why matched: Airworthiness Directives; Honeywell International Inc. (Formerly AlliedSignal, Inc., Formerly Textron Lycoming, Formerly Avco Lycoming) T5309, T5311, T5313B, T5317A, T5317A-1, and T5317B Series, and T53-L-9, T53-L-11, T53-L-13B, T53-L-13BA, T53-L-13B S/SA, T53-L-13B S/SB, T53-L- 13B/D, and T53-L-703 Series Turboshaft Engines

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

2005-13-07

final rule

Airworthiness Directives; Honeywell International Inc. (Formerly AlliedSignal Inc. and Garrett Turbine Engine Co.) TFE731-2 and -3 Series Turbofan Engines

Unsafe Condition: could result in an uncontained engine failure and damage to the airplane.

Effective: Jul 27, 2005 Category: engine

Why matched: Airworthiness Directives; Honeywell International Inc. (Formerly AlliedSignal Inc. and Garrett Turbine Engine Co.) TFE731-2 and -3 Series Turbofan Engines

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

2004-09-29 Recurring

final rule

Airworthiness Directives; Honeywell International Inc. (Formerly AlliedSignal Inc., Garrett Turbine Engine Company, and AiResearch Manufacturing Company of Arizona) TPE331-10 and -11 Series Turboprop Engines

Unsafe Condition: The FAA is adopting a new airworthiness directive (AD) for Honeywell International Inc. (formerly AlliedSignal Inc., Garrett Turbine Engine Company, and AiResearch Manufacturing Company of Arizona)...

Effective: Jun 15, 2004 Category: engine

Why matched: Airworthiness Directives; Honeywell International Inc. (Formerly AlliedSignal Inc., Garrett Turbine Engine Company, and AiResearch Manufacturing Company of Arizona) TPE331-10 and -11 Series Turboprop Engines

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

2003-15-07

final rule

Airworthiness Directives; Honeywell International Inc. (Formerly AlliedSignal) Model RE220 (RJ) Auxiliary Power Units

Unsafe Condition: Cracks occurring in the existing APU fuel nozzles leading to fuel leaks.

Effective: Sep 3, 2003 Category: aircraft Compliance: Within six months after the effective date of this AD.

Why matched: Airworthiness Directives; Honeywell International Inc. (Formerly AlliedSignal) Model RE220 (RJ) Auxiliary Power Units

2003-02-01

final rule

Airworthiness Directives; Honeywell International, Inc., (formerly AlliedSignal, Inc. and Textron Lycoming) ALF502L-2, ALF502L-2C, ALF502R-3 and ALF502R-3A Series Turbofan Engines

Unsafe Condition: Fracture of the flow divider left primary fuel tube due to high-cycle fatigue resulting from a missing support clamp.

Effective: Jan 30, 2003 Category: engine Compliance: Before further flight.

Why matched: Airworthiness Directives; Honeywell International, Inc., (formerly AlliedSignal, Inc. and Textron Lycoming) ALF502L-2, ALF502L- 2C, ALF502R-3 and ALF502R-3A Series Turbofan Engines

2002-22-06 Recurring

final rule

Airworthiness Directives; Honeywell International, Inc., (Formerly AlliedSignal, Inc. and Textron Lycoming) LF507 and ALF502R Series Turbofan Engines

Unsafe Condition: Separation of the combustor dome baffle from the combustion chamber liner assembly, leading to engine combustion chamber liner assembly burn through.

Effective: Nov 18, 2002 Category: engine Compliance: Not specified in the source.

Why matched: Airworthiness Directives; Honeywell International, Inc., (Formerly AlliedSignal, Inc. and Textron Lycoming) LF507 and ALF502R Series Turbofan Engines

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

2002-15-04 Recurring

final rule

Airworthiness Directives; Honeywell International, Inc., (formerly AlliedSignal, Inc. and Textron Lycoming) T5313B, T5317 Series, and T53 Series Turboshaft Engines

Unsafe Condition: Centrifugal compressor impellers may have been inadvertently misidentified, potentially leading to operation beyond their design service life, which could result in premature failure, uncontained e...

Effective: Sep 10, 2002 Category: engine Compliance: Before further flight

Why matched: Airworthiness Directives; Honeywell International, Inc., (formerly AlliedSignal, Inc. and Textron Lycoming) T5313B, T5317 Series, and T53 Series Turboshaft Engines

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

2002-12-08

final rule

Airworthiness Directives; Honeywell International, Inc. (formerly AlliedSignal Inc., and Textron Lycoming) ALF502 and LF507 Series Turbofan Engines

Unsafe Condition: Continuous analysis of field-returned hardware indicates smaller service life margins than originally expected, which could lead to GPT component failure and an uncontained engine failure.

Effective: Jul 17, 2002 Category: engine Compliance: Before further flight

Why matched: Airworthiness Directives; Honeywell International, Inc. (formerly AlliedSignal Inc., and Textron Lycoming) ALF502 and LF507 Series Turbofan Engines

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

2002-12-09 Recurring

final rule

Airworthiness Directives; Honeywell International Inc. (Formerly AlliedSignal Inc. and Garrett Turbine Engine Company) TPE331-11U, -12B, -12JR, -12UA, -12UAR, and -12UHR Series Turboprop Engines

Unsafe Condition: Reports of spur gearshaft (bull gear) rim separations and high-speed pinion (HSP) assembly failures.

Effective: Jul 3, 2002 Category: engine Compliance: Not specified in the provided text.

Why matched: Airworthiness Directives; Honeywell International Inc. (Formerly AlliedSignal Inc. and Garrett Turbine Engine Company) TPE331-11U, -12B, -12JR, -12UA, -12UAR, and -12UHR Series Turboprop Engines

2002-09-09 Recurring

final rule

Airworthiness Directives; Honeywell International, Inc., (Formerly AlliedSignal, Inc., Textron Lycoming, Avco Lycoming, and Lycoming) Former Military T53 Series Turboshaft Engines

Unsafe Condition: Low-cycle fatigue failure of the centrifugal compressor impeller, resulting in an uncontained engine failure.

Effective: Jun 13, 2002 Category: engine Compliance: Before further flight.

Why matched: Airworthiness Directives; Honeywell International, Inc., (Formerly AlliedSignal, Inc., Textron Lycoming, Avco Lycoming, and Lycoming) Former Military T53 Series Turboshaft Engines

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

2002-03-09 R1

final rule

Airworthiness Directives; Honeywell International Inc. (formerly AlliedSignal Inc. and Textron Lycoming) LTS101 Series Turboshaft and LTP101 Series Turboprop Engines

Unsafe Condition: Impeller failure from cracks in the impeller back face area, which could result in an uncontained engine failure.

Effective: Mar 27, 2002 Category: engine Compliance: Within 900 gas generator (Ng) cycles after the effective date of this AD.

Why matched: Airworthiness Directives; Honeywell International Inc. (formerly AlliedSignal Inc. and Textron Lycoming) LTS101 Series Turboshaft and LTP101 Series Turboprop Engines

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

2002-03-09

final rule

Airworthiness Directives; Honeywell International Inc. (Formerly AlliedSignal Inc. and Textron Lycoming) LTS101 Series Turboshaft and LTP101 Series Turboprop Engines

Unsafe Condition: A machining discrepancy during manufacture of certain impellers may result in cracks in the impeller back face area, potentially leading to impeller failure and an uncontained engine failure.

Effective: Mar 27, 2002 Category: engine Compliance: Before further flight

Why matched: Airworthiness Directives; Honeywell International Inc. (Formerly AlliedSignal Inc. and Textron Lycoming) LTS101 Series Turboshaft and LTP101 Series Turboprop Engines

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

Amdt-39-12676

final rule

Airworthiness Directives; Honeywell International Inc. (formerly AlliedSignal Inc. and Textron Lycoming) LTS101 Series Turboshaft and LTP101 Series Turboprop Engines

Unsafe Condition: Impeller failure from cracks in the impeller back face area, which could result in an uncontained engine failure.

Effective: Mar 27, 2002 Category: engine Compliance: Before further flight

Why matched: Airworthiness Directives; Honeywell International Inc. (formerly AlliedSignal Inc. and Textron Lycoming) LTS101 Series Turboshaft and LTP101 Series Turboprop Engines

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

2002-03-01 Recurring

final rule

Airworthiness Directives; Honeywell International, Inc., (Formerly AlliedSignal, Inc., and Textron Lycoming) T5311A, T5311B, T5313B, T5317A, T5317B, T53-L-11, T53-L-11A, T53-L-11B, T53-L-11C, T53-L-11D, T53-L-11A S/SA, T53-L-13B, T53-L-13B S/SA, T53-L-13B S/SB, and T53-L-703 Turboshaft Engines

Unsafe Condition: Tachometer drive spur gear failure, potentially leading to engine overspeed, loss of power turbine speed (N2) instrument panel indication, and hard landings.

Effective: Mar 21, 2002 Category: engine Compliance: Before further flight

Why matched: Airworthiness Directives; Honeywell International, Inc., (Formerly AlliedSignal, Inc., and Textron Lycoming) T5311A, T5311B, T5313B, T5317A, T5317B, T53-L-11, T53-L-11A, T53-L-11B, T53-L-11C, T53-L-11D, T53-L-11A S/SA, T53-L-13B, T53-L-13B S/SA, T53-L-13B S/SB, and T53-L-703 Turboshaft Engines

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

2001-21-02

final rule

Airworthiness Directives; Honeywell International Inc. (formerly AlliedSignal Inc. and Garrett Turbine Engine Company) TPE331-8, -10N, and -12B Turboprop Engines

Unsafe Condition: Uncommanded torque increase to 150% within 5 seconds of initial torque acceleration, leading to asymmetric thrust and potential loss of control.

Effective: Nov 19, 2001 Category: engine Compliance: Within 30 days after the effective date of the AD.

Why matched: Airworthiness Directives; Honeywell International Inc. (formerly AlliedSignal Inc. and Garrett Turbine Engine Company) TPE331-8, -10N, and -12B Turboprop Engines

2001-17-15 Recurring

final rule

Airworthiness Directives; Honeywell International Inc. (formerly AlliedSignal Inc. and Textron Lycoming Inc.) LTS101 Series Turboshaft and LTP101 Series Turboprop Engines

Unsafe Condition: Worn splines in fuel pumps which could cause engine fuel pump failure, resulting in total engine power loss and possible loss of the aircraft.

Effective: Oct 1, 2001 Category: aircraft Compliance: Within specified time-in-service (TIS) intervals after the effective date of the AD.

Why matched: Airworthiness Directives; Honeywell International Inc. (formerly AlliedSignal Inc. and Textron Lycoming Inc.) LTS101 Series Turboshaft and LTP101 Series Turboprop Engines

2000-11-15

final rule

Airworthiness Directives; Honeywell International Inc. (Formerly AlliedSignal Inc.) ALF502R and LF507 Series Turbofan Engines

Unsafe Condition: Uncontained failures of critical rotating engine parts, which could result in damage to the airplane.

Effective: Jul 10, 2000 Category: engine Compliance: Within 60 days after the effective date of this AD.

Why matched: Airworthiness Directives; Honeywell International Inc. (formerly AlliedSignal Inc.) ALF502R and LF507 Series Turbofan Engines

00-5009

final rule

Airworthiness Directives; Honeywell International (formerly AlliedSignal Inc.) 36-300(A), 36-280(B), and 36-280(D) Series Auxiliary Power Units

Unsafe Condition: Reports of load compressor impeller failures have been received, which could lead to an uncontained APU failure and damage to the airplane.

Effective: May 8, 2000 Category: aircraft Compliance: Before further flight.
Technical illustration of an aircraft turbine engine assembly
Problem area Engine

2000-04-24

final rule

Airworthiness Directives; Honeywell International (formerly AlliedSignal Inc.) 36-300(A), 36-280(B), and 36-280(D) Series Auxiliary Power Units

Unsafe Condition: Auxiliary Power Units

Effective: May 8, 2000 Category: appliance

Why matched: Airworthiness Directives; Honeywell International (formerly AlliedSignal Inc.) 36-300(A), 36-280(B), and 36-280(D) Series Auxiliary Power Units

2000-05-14 Recurring

final rule

Airworthiness Directives; AlliedSignal Inc. ALF502 and LF507 Series Turbofan Engines

Unsafe Condition: This amendment supersedes two existing airworthiness directives (AD's), applicable to AlliedSignal Inc. ALF502 and LF507 series turbofan engines, that require rework or replacement of No. 4 and 5 b...

Effective: Apr 27, 2000 Category: engine

Why matched: Airworthiness Directives; AlliedSignal Inc. ALF502 and LF507 Series Turbofan Engines

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

00-6158

final rule

Airworthiness Directives; British Aerospace Model BAe 146-100A, - 200A, and -300A Series Airplanes Equipped With AlliedSignal ALF502R- Series Engines

Unsafe Condition: Uncommanded engine thrust reductions (rollback) when operating in certain icing conditions near thunderstorms.

Effective: Apr 24, 2000 Category: engine Compliance: Before further flight

Why matched: Airworthiness Directives; British Aerospace Model BAe 146-100A, - 200A, and -300A Series Airplanes Equipped With AlliedSignal ALF502R- Series Engines