Airbus | The Boeing Company | Garrett Auxiliary Power Division Airworthiness Directives

40 ADs indexed for Airbus | The Boeing Company | Garrett Auxiliary Power Division aircraft.

Models

Recent ADs

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

2002-12-09 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

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

Amdt-39-10327

final rule

Airworthiness Directives; AlliedSignal Inc. TPE331 Series Turboprop and TSE331 Turboshaft Engines

Unsafe Condition: Third stage turbine wheel separation due to thermal fatigue cracking and shifting of the third stage turbine stator, which could contact the third stage turbine wheel and result in an uncontained e...

Effective: Apr 27, 1998 Category: engine Compliance: Before further flight

Why matched: Airworthiness Directives; AlliedSignal Inc. TPE331 Series Turboprop and TSE331 Turboshaft Engines

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

Amdt-39-10084

final rule

Airworthiness Directives; AlliedSignal Inc. TPE331 Series Turboprop Engines

Unsafe Condition: Icing of the inlet Pt2 sensor can produce an erroneous (high) pressure signal to the fuel control, causing little or no response to power lever movement.

Effective: Sep 22, 1997 Category: engine Compliance: Before further flight

Why matched: Airworthiness Directives; AlliedSignal Inc. TPE331 Series Turboprop Engines

Amdt-39-9181

final rule

Airworthiness Directives; AlliedSignal Inc. TFE731-3 Series Turbofan Engines

Unsafe Condition: LPT disks may separate through the disk web due to creep fatigue, which may result in an uncontained engine failure.

Effective: Jun 19, 1995 Category: engine Compliance: Before further flight

Why matched: Airworthiness Directives; AlliedSignal Inc. TFE731-3 Series Turbofan Engines

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

Amdt-39-9182

final rule

Airworthiness Directives; AlliedSignal Aerospace GTCP85 Series Auxiliary Power Units

Unsafe Condition: Uncontained APU failures where turbine wheel fragments exit the APU exhaust axially and damage the aircraft.

Effective: May 3, 1995 Category: engine Compliance: Before further flight

Why matched: Airworthiness Directives; AlliedSignal Aerospace GTCP85 Series Auxiliary Power Units

94-23-04

final rule

Airworthiness Directives; Garrett Turbine Engine Company ATF3 Series Turbofan Engines

Unsafe Condition: Cracks in the curvic and bore area of the high pressure turbine (HPT) rotor assembly disk could lead to an uncontained failure of the HPT rotor assembly disk.

Effective: Feb 6, 1995 Category: engine Compliance: Within 50 cycles in service (CIS) after the effective date for engines with 1550 or more HPT roto...

Why matched: Airworthiness Directives; Garrett Turbine Engine Company ATF3 Series Turbofan Engines

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

94-09-08

final rule

ALLIED-SIGNAL INC., GARRETT ENGINE DIVISION Model TPE331-1, -2, -2UA, -3U, -3UW, -5, - 5A, -6, and -6A and TSE331-3U Engines

Unsafe Condition: Third stage turbine stator assemblies assembled with inner seal supports made of incorrect material (Hastelloy S) result in significantly reduced cyclic life and potential fatigue failure, leading ...

Effective: May 20, 1994 Category: engine Compliance: Within specified cycles in service after the effective date of this AD (May 20, 1994), based on c...

Why matched: ALLIED-SIGNAL INC., GARRETT ENGINE DIVISION Model TPE331-1, -2, -2UA, -3U, -3UW, -5, - 5A, -6, and -6A and TSE331-3U Engines

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

93-15-11

final rule

ALLIED-SIGNAL INC., GARRETT ENGINE DIVISION Model TPE331-47A, -55B, and -61A and TPE331-1, -2, -3, -5, -6, -8, -10, -11, -12, -14A, -14B, -15AW, -25, and -43 Series Engines

Unsafe Condition: Sudden loss of propeller control during application of thrust reverse that may cause asymmetric thrust and loss of aircraft control.

Effective: Sep 7, 1993 Category: engine Compliance: Within the next 10 hours time in service (TIS) after the effective date of this AD

Why matched: ALLIED-SIGNAL INC., GARRETT ENGINE DIVISION Model TPE331-47A, -55B, and -61A and TPE331-1, -2, -3, -5, -6, -8, -10, -11, -12, -14A, -14B, -15AW, -25, and -43 Series Engines

Technical illustration of an aircraft propeller assembly
Problem area Propeller

92-26-08

final rule

ALLIED-SIGNAL INC., GARRETT ENGINE DIVISION Model TPE331-1, -2, -2UA, -3U, -3UW, -5, -5A, -6, -6A and TSE331-3U Engines

Unsafe Condition: Cracking of third stage stator assemblies, which could lead to an uncontained failure of the third stage turbine wheel.

Effective: Jul 15, 1993 Category: engine Compliance: Within 50 cycles in service after the effective date for 900+ cycles; within 150 cycles but not e...

Why matched: ALLIED-SIGNAL INC., GARRETT ENGINE DIVISION Model TPE331-1, -2, -2UA, -3U, -3UW, -5, -5A, -6, -6A and TSE331-3U Engines

93-05-09

final rule

ALLIED-SIGNAL INC., GARRETT ENGINE DIVISION Model TPE331-1, -2, -2UA, -3U, -3UW, -5, -5A, -5AB, -5B, -6, and -6A, and TSE331-3U Engines

Unsafe Condition: Failure of the third stage turbine wheel due to insufficient cycles in service (CIS) limits on third stage turbine stator assemblies Part Number 868379-1, -3, or -5.

Effective: Jun 28, 1993 Category: engine Compliance: Required as indicated, unless accomplished previously.

Why matched: ALLIED-SIGNAL INC., GARRETT ENGINE DIVISION Model TPE331-1, -2, -2UA, -3U, -3UW, -5, -5A, -5AB, -5B, -6, and -6A, and TSE331-3U Engines

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

93-02-01

final rule

GARRETT ENGINE DIVISION, ALLIED-SIGNAL INCORPORATED Model TPE331-8, -10, -11, and -12 Series Engines

Unsafe Condition: Fuel spraying on hot turbine components can result in an engine fire.

Effective: Mar 18, 1993 Category: engine Compliance: Within the next 50 hours time in service after the effective date of this AD

Why matched: GARRETT ENGINE DIVISION, ALLIED-SIGNAL INCORPORATED Model TPE331-8, -10, -11, and -12 Series Engines

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

92-02-18

final rule

GARRETT ENGINE DIVISION, ALLIED-SIGNAL INCORPORATED Model TFE731-5BR Engines

Unsafe Condition: Multiple inflight engine failures due to engines identified as Part Number 3075330-2 or 3075370-1.

Effective: Feb 10, 1993 Category: engine Compliance: Required prior to further flight, unless accomplished previously.

Why matched: GARRETT ENGINE DIVISION, ALLIED-SIGNAL INCORPORATED Model TFE731-5BR Engines

92-21-06

final rule

GARRETT ENGINE DIVISION, A DIVISION OF THE ALLIED SIGNAL AEROSPACE COMPANY Model TFE731-2, -3, -3A, -3AR, and -3R Engines

Unsafe Condition: Low Pressure Turbine (LPT) Rotor Disks with specified part numbers and serial numbers listed in ASB TFE731-A72-3474 may cause an uncontained engine failure.

Effective: Nov 27, 1992 Category: engine Compliance: next access to the turbine rotor assembly or before accumulating 100 hours time in service after ...

Why matched: GARRETT ENGINE DIVISION, A DIVISION OF THE ALLIED SIGNAL AEROSPACE COMPANY Model TFE731-2, -3, -3A, -3AR, and -3R Engines

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

92-21-05

final rule

Airworthiness Directives; GARRETT AUXILIARY POWER DIVISION Model GTCP 36-300 Auxiliary Power Units

Unsafe Condition: Damage to the titanium APU fire wall due to APU tieshaft separation, which could lead to a reduction in the fire protection capability of the APU compartment.

Effective: Nov 24, 1992 Category: appliance Compliance: Within 30 months after the effective date of this AD

Why matched: Airworthiness Directives; GARRETT AUXILIARY POWER DIVISION Model GTCP 36-300 Auxiliary Power Units

92-16-06

final rule

Airworthiness Directives; GARRETT AIRRESEARCH All Aircraft Equipped with Garrett AirResearch AircraftStarters that are Installed in, but not limited to, Boeing Models 707, 727, and 737 Airplanes and McDonnell Douglas Models DC-8, DC-9, and DC-10 Airplanes

Unsafe Condition: In-service fatigue or structural failures of the aircraft starter could result in an in-flight fire or loss of control of the airplane.

Effective: Aug 31, 1992 Category: appliance Compliance: Within the next 90 calendar days after the effective date of this AD for the inspection, and with...

Why matched: Airworthiness Directives; GARRETT AIRRESEARCH All Aircraft Equipped with Garrett AirResearch AircraftStarters that are Installed in, but not limited to, Boeing Models 707, 727, and 737 Airplanes and McDonnell Douglas Models DC-8, DC-9, and DC-10 Airplanes

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