Allied Ag Cat Productions, Inc. Airworthiness Directives

137 ADs indexed for Allied Ag Cat Productions, Inc. aircraft.

Models

G-164A 18 ADs G-164B 15 ADs G-164B (with 73 inch wing gap) 15 ADs G-164B-15T 15 ADs G-164B-20T 15 ADs G-164B-34T 15 ADs G-164 14 ADs G-164C 10 ADs G-164D 9 ADs G-164D (with 73 inch wing gap) 9 ADs Various 6 ADs TFE731 4 ADs G-164A 3 ADs G-164B 3 ADs A300 B2-1A 2 ADs A300 B2-1C 2 ADs A300 B2-203 2 ADs A300 B2K-3C 2 ADs A300 B4-103 2 ADs A300 B4-203 2 ADs A300 B4-2C 2 ADs A300 B4-601 2 ADs A300 B4-603 2 ADs A300 B4-605R 2 ADs Ag Cat Productions, Inc. (Type Certificate No. 1A16 Formerly Held by Schweizer 2 ADs G-164 2 ADs G-164B (with 73 inch wing gap) 2 ADs G-164B-15T 2 ADs G-164B-20T 2 ADs G-164B-34T 2 ADs G-164C 2 ADs G-164D 2 ADs G-164D (with 73 inch wing gap) 2 ADs TFE731-40R-200G 2 ADs 707-100 Long Body 1 AD 707-100B Long Body 1 AD 707-100B Short Body 1 AD 707-200 1 AD 707-300 Series 1 AD 707-300B Series 1 AD 707-300C Series 1 AD Auxiliary Power Units 1 AD BAC 1-11 200 Series 1 AD BAC 1-11 400 Series 1 AD A340-211 1 AD A340-212 1 AD A340-213 1 AD A340-311 1 AD A340-312 1 AD A340-313 1 AD A340-541 1 AD A340-642 1 AD ATR42-200 1 AD Traffic Alert and Collision Avoidance System II processors 1 AD A300 B2-1A 1 AD A300 B2-1C 1 AD A300 B2-203 1 AD A300 B2K-3C 1 AD A300 B4-103 1 AD A300 B4-203 1 AD A300 B4-2C 1 AD A300 B4-601 1 AD A300 B4-603 1 AD A300 B4-605R 1 AD A300 B2-1A 1 AD A300 B2-1C 1 AD A300 B2-203 1 AD A300 B2K-3C 1 AD A300 B4-103 1 AD A300 B4-203 1 AD A300 B4-2C 1 AD A300 B4-601 1 AD A300 B4-603 1 AD A300 B4-605R 1 AD Ag Cat Productions, Inc. 1 AD Ag Cat Productions, Inc. Models G-164, G-164A, G-164B, G-164B With 73″ Wing Gap, G-164B-15T, G-164B-34T, G-164B-20T, G-164C, G-164D, and G-164D With 73″ Wing Gap 1 AD ALF502 LF507 1 AD TPE331 1 AD Various 1 AD 31A 1 AD ATP 1 AD F27 Mark 050 1 AD Navigation Receivers 1 AD 200 1 AD 200C 1 AD 200CT 1 AD 200T 1 AD 300 1 AD Autopilot Servo Actuators 1 AD Mystere-Falcon 20 - C5 1 AD Mystere-Falcon 20 - D5 1 AD Mystere-Falcon 20 - E5 1 AD Mystere-Falcon 20 - F5 1 AD 525 1 AD 550 1 AD 560 1 AD Avro 146-RJ100A 1 AD BAe 146-200A 1 AD Falcon 10 1 AD Jetstream Model 4101 1 AD Mystere-Falcon 20 - C5 1 AD Mystere-Falcon 20 - D5 1 AD Mystere-Falcon 20 - E5 1 AD

Recent ADs

2023-08-07

final rule

Airworthiness Directives; Allied Ag Cat Productions, Inc. Airplanes

Unsafe Condition: detachment of the airplane's propeller pitch control linkage from the PPC of the engine

Effective: Jun 21, 2023 Category: engine Compliance: Within 50 flight hours

Why matched: Airworthiness Directives; Allied Ag Cat Productions, Inc. Airplanes

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

2011-05-07 Recurring

final rule

Airworthiness Directives; Allied Ag Cat Productions, Inc. Models G-164, G-164A, G-164B, G-164B With 73″ Wing Gap, G-164B-15T, G-164B-34T, G-164B-20T, G-164C, G-164D, and G-164D With 73″ Wing Gap Airplanes

Unsafe Condition: Corrosion in the rudder main tubular spar could result in failure of the rudder main spar tube, leading to loss of directional control.

Effective: Mar 17, 2011 Category: aircraft Compliance: Within 5 years of the effective date of this AD for Models G-164, G-164A, and G-164B airplanes.

Why matched: Airworthiness Directives; Allied Ag Cat Productions, Inc. Models G-164, G-164A, G-164B, G-164B With 73'' Wing Gap, G-164B-15T, G-164B- 34T, G-164B-20T, G-164C, G-164D, and G-164D With 73'' Wing Gap Airplanes

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

2008-22-21 Recurring

final rule

Airworthiness Directives; Allied Ag Cat Productions, Inc. Model G-164 Series Airplanes

Unsafe Condition: Corrosion in the rudder main tubular spar could result in failure of the weld to the main spar tube, leading to loss of directional control.

Effective: Dec 19, 2008 Category: aircraft Compliance: Initially inspect within the next 60 months after the last inspection required in AD 78-08-09 or ...

Why matched: Airworthiness Directives; Allied Ag Cat Productions, Inc. Model G-164 Series Airplanes

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

2007-17-02

final rule

Airworthiness Directives; Allied Ag Cat Productions, Inc. (Type Certificate No. 1A16 Formerly Held by Schweizer Aircraft Corp.) G-164 Series Airplanes

Unsafe Condition: Turning the fuel shut-off valve clockwise past the 'ON' position, which could allow the fuel valve to be rotated to an unplacarded 'OFF' position, leading to reduced fuel flow and consequent loss o...

Effective: Sep 18, 2007 Category: aircraft Compliance: Within the next 100 hours time-in-service after the applicable effective date (April 6, 1982 for ...

Why matched: Airworthiness Directives; Allied Ag Cat Productions, Inc. (Type Certificate No. 1A16 Formerly Held by Schweizer Aircraft Corp.) G-164 Series Airplanes

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

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

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