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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

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

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

2002-03-09 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

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

Amdt-39-11332

final rule

Airworthiness Directives; AlliedSignal Inc. TFE731 Series Turbofan Engines

Unsafe Condition: Cracking of the fuel tube and subsequent leakage of fuel on or around electrical components, which can cause an engine fire.

Effective: Nov 29, 1999 Category: engine

Why matched: Airworthiness Directives; AlliedSignal Inc. TFE731 Series Turbofan Engines

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

Amdt-39-11225

final rule

Airworthiness Directives; AlliedSignal Inc. (Formerly Textron Lycoming) Model ALF502R-5 and ALF502R-3A Turborfan Engines

Unsafe Condition: Reports of uncommanded reduction of engine thrust (rollback) and loss of thrust control in icing conditions.

Effective: Sep 17, 1999 Category: engine Compliance: Before further flight.

Why matched: Airworthiness Directives; AlliedSignal Inc. (Formerly Textron Lycoming) Model ALF502R-5 and ALF502R-3A Turborfan Engines

99-15-06

final rule

Airworthiness Directives; AlliedSignal Inc. (formerly Textron Lycoming) Model ALF502R-5 and ALF502R-3A Turbofan Engines

Unsafe Condition: Ice accretion on the fan core inlet stator vane surfaces can result in engine rollback and loss of thrust control in icing conditions.

Effective: Sep 17, 1999 Category: engine Compliance: Before further flight, but no later than December 31, 2002.

Why matched: Airworthiness Directives; AlliedSignal Inc. (formerly Textron Lycoming) Model ALF502R-5 and ALF502R-3A Turbofan Engines

99-12-06

final rule

Airworthiness Directives; AlliedSignal Inc. VN 411B Very High Frequency (VHF) Navigation Receivers

Unsafe Condition: VHF navigation receiver interference from frequency modulation (FM) radio station broadcast frequencies could cause distortion of the navigation audio and deflection of the desired flight path duri...

Effective: Jul 23, 1999 Category: appliance Compliance: Within 90 calendar days after the effective date (July 23, 1999) or upon replacement/repair of th...

Why matched: Airworthiness Directives; AlliedSignal Inc. VN 411B Very High Frequency (VHF) Navigation Receivers

Amdt-39-11190

final rule

Airworthiness Directives; AlliedSignal Inc. VN 411B Very High Frequency (VHF) Navigation Receivers

Unsafe Condition: Navigation receiver interference during landing operations caused by frequency modulation (FM) radio station broadcasts, leading to distortion of navigation audio and deflection of the desired flig...

Effective: Jul 23, 1999 Category: aircraft Compliance: Before further flight.

98-17-01 R1

final rule

Airworthiness Directives; AlliedSignal Inc. TFE731 Series Turbofan Engines

Unsafe Condition: Cracked fuel tubes and subsequent leakage of fuel on or around electrical components, which can cause an engine fire.

Effective: May 19, 1999 Category: engine Compliance: Within 160 hours time-in-service after the effective date or prior to December 20, 1999, whicheve...

Why matched: Airworthiness Directives; AlliedSignal Inc. TFE731 Series Turbofan Engines

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

99-07-19

final rule

Airworthiness Directives; AlliedSignal Inc. TFE731-40R-200G Turbofan Engines

Unsafe Condition: Fuel flow meter tube assembly part number 3061157-2 failures causing fuel spraying on electrical components due to cracked fuel lines, leading to in-flight engine shutdowns and potential engine fires.

Effective: Apr 21, 1999 Category: engine Compliance: Within 30 days of effective date for replacement actions; inspections due within 5 or 25 hours ti...

Why matched: Airworthiness Directives; AlliedSignal Inc. TFE731-40R-200G Turbofan Engines

Amdt-39-11103

final rule

Airworthiness Directives; AlliedSignal Inc. TFE731-40R-200G Turbofan Engines

Unsafe Condition: Failure of the fuel flow meter tube assembly part number 3061157-2, leading to fuel spraying on and around electrical components due to a cracked fuel line, which can cause in-flight engine shutdow...

Effective: Apr 21, 1999 Category: engine Compliance: Before further flight

Why matched: Airworthiness Directives; AlliedSignal Inc. TFE731-40R-200G Turbofan Engines

Amdt-39-10703

final rule

Airworthiness Directives; AlliedSignal Inc. TFE731 Series Turbofan Engines

Unsafe Condition: Cracking of the fuel tube can cause fuel leakage on or around electrical components, which can cause an engine fire.

Effective: Oct 13, 1998 Category: engine Compliance: Before further flight

Why matched: Airworthiness Directives; AlliedSignal Inc. TFE731 Series Turbofan Engines

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

Amdt-39-10637

final rule

Airworthiness Directives; AlliedSignal Inc. KT 76A Air Traffic Control (ATC) Transponders

Unsafe Condition: The KT 76A ATC transponders may transmit misleading encoding altimeter information to ground-based ATC radar sites and nearby TCAS-equipped aircraft due to inability to coordinate.

Effective: Aug 16, 1998 Category: aircraft Compliance: Before further flight