Twin Commander Aircraft LLC Airworthiness Directives

125 ADs indexed for Twin Commander Aircraft LLC aircraft.

Models

690A 20 ADs 690 17 ADs 690B 16 ADs 680 15 ADs 560-A 14 ADs 560-E 13 ADs 680-E 13 ADs 720 13 ADs 500 12 ADs 520 12 ADs 560 12 ADs 680-F 11 ADs 500-A 10 ADs 500-B 10 ADs 680-FL(P) 10 ADs 685 10 ADs 690C 10 ADs 690D 10 ADs 695 10 ADs 695A 10 ADs 500-S 9 ADs 500-U 9 ADs 560-F 9 ADs 680-FL 9 ADs 681 9 ADs 680-F(P) 8 ADs 680-V 8 ADs 680-W 8 ADs Various 7 ADs 680-T 7 ADs 695B 7 ADs Commander 5 ADs F.260 1 AD F.260B 1 AD F.260C 1 AD F.260D 1 AD F.260E 1 AD F.260F 1 AD S.205 - 18/F 1 AD S.205 - 18/R 1 AD S.205 - 20/F 1 AD S.205 - 20/R 1 AD AT-302 1 AD AT-400 1 AD BN-2 1 AD BN-2A 1 AD BN-2A-3 1 AD H.P. 137 Jetstream Mk. 1 1 AD Nord 262A Series 1 AD PA-60-600 (Aerostar 600) 1 AD PA-60-601 (Aerostar 601) 1 AD PA-60-601P (Aerostar 601P) 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 A 1 AD A-2 1 AD A-3 1 AD A-4 1 AD A-5 1 AD A-5T 1 AD A-6 1 AD A-7 1 AD A-7T 1 AD A-9 1 AD 150G 1 AD 172H (USAF T-41A) 1 AD 180H 1 AD 182J 1 AD 182K 1 AD 185E 1 AD 188 1 AD 206A 1 AD 210F 1 AD 210G 1 AD 120 1 AD 140 1 AD 140A 1 AD 150 1 AD 150A 1 AD 150B 1 AD 150C 1 AD 150D 1 AD 150E 1 AD CH-300 Pacemaker 1 AD 172 1 AD 172A 1 AD 172B 1 AD 172C 1 AD 172D 1 AD 172E 1 AD 172F (USAF T-41A) 1 AD 172G 1 AD 172H (USAF T-41A) 1 AD 172I 1 AD 180 1 AD 182 1 AD 185 1 AD 188 1 AD 206 1 AD 207 1 AD 210 1 AD 310 1 AD 320 1 AD 340 1 AD 328-100 1 AD F.260 1 AD F.260B 1 AD F.260C 1 AD F.260D 1 AD F.260E 1 AD GTX 33 1 AD GTX 330 1 AD GTX 330D 1 AD GTX 33D 1 AD F-401 1 AD F-5 1 AD 60 1 AD 95-C55 1 AD 95-C55A 1 AD A36 1 AD A60 1 AD B60 1 AD D55 1 AD D55A 1 AD E55 1 AD E55A 1 AD 35 1 AD 500A 1 AD 500B 1 AD 500S 1 AD 500U 1 AD H35 1 AD Hose Assemblies 1 AD J35 1 AD K35 1 AD M35 1 AD 700 1 AD

Recent ADs

2023-09-09 Recurring

final rule

Airworthiness Directives; Various Airplanes, Helicopters, and Engines

Unsafe Condition: Multiple failures of spot-welded, multi-segment v-band couplings at the tailpipe to the turbocharger exhaust housing flange.

Effective: Jul 17, 2023 Category: engine Compliance: Within 50 flight hours after the effective date of this AD.

Why matched: Airworthiness Directives; Various Airplanes, Helicopters, and Engines

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

2022-03-15

final rule

Airworthiness Directives; Various Airplanes

Unsafe Condition: The displayed fuel quantity can have an error as much as four gallons/fuel tank with the display indicating four gallons with an empty tank. In the context of this event, the end level effect is th...

Effective: Mar 21, 2022 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Various Airplanes

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

2013-09-05

final rule

Airworthiness Directives; Twin Commander Aircraft LLC Airplanes

Unsafe Condition: Cracking of the outer fuselage attachments, the lower wing main spar, the vertical channels, the upper picture window channels, aft cabin pressure web, external wing to fuselage fillets, and fasten...

Effective: May 29, 2013 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Twin Commander Aircraft LLC Airplanes

Technical illustration of a riveted aircraft structural panel and frame
Problem area Airframe structure

84-10-07

final rule

Airworthiness Directives; Gulfstream Model 680T, 680V, 680W and Model 681 Series Airplanes

Unsafe Condition: Failure of the emergency landing gear extension system could result in inability to extend the landing gear during an emergency.

Effective: Jun 23, 2011 Category: aircraft Compliance: within the next 100 hours time-in-service after the effective date of this AD unless already acco...

Why matched: Airworthiness Directives; Gulfstream Model 680T, 680V, 680W and Model 681 Series Airplanes

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

2011-09-19

final rule

Airworthiness Directives; BURKHART GROB LUFT-UND Model G 103 C Twin III SL Gliders

Unsafe Condition: The in-flight loss of a propeller and pulley wheel from the engine of a Grob G 103 C Twin III SL powered sailplane has been reported. Grob Aircraft AG suspects that the possible reasons for this lo...

Effective: Jun 15, 2011 Category: aircraft Compliance: Within 30 days after the effective date of this AD (June 15, 2011).

Why matched: Airworthiness Directives; BURKHART GROB LUFT-UND Model G 103 C Twin III SL Gliders

2010-11-02

final rule

Airworthiness Directives; Gulfstream Aerospace LP (Type Certificate Previously Held by Israel Aircraft Industries, Ltd.) Model Gulfstream 100 Airplanes, and Model Astra SPX and 1125 Westwind Astra Airplanes

Unsafe Condition: Incomplete closure of the Main Entry Door (MED) may be followed by in-flight opening of the door. As a result, the MED and the adjacent fuselage structure may be damaged during opening and landing ...

Effective: Jun 25, 2010 Category: aircraft Compliance: Within 10 days after February 15, 2007 (the effective date of AD 2007-03-05).

Why matched: Airworthiness Directives; Gulfstream Aerospace LP (Type Certificate Previously Held by Israel Aircraft Industries, Ltd.) Model Gulfstream 100 Airplanes, and Model Astra SPX and 1125 Westwind Astra Airplanes

Technical illustration of a riveted aircraft structural panel and frame
Problem area Airframe structure

2009-25-02

final rule

Airworthiness Directives; Twin Commander Aircraft LLC Models 690, 690A, and 690B Airplanes

Unsafe Condition: Corrosion between the mating surfaces of the wing upper skin surface and the engine mount beam support straps could result in failure of the engine mount beam support straps, leading to loss of the...

Effective: Jan 8, 2010 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Twin Commander Aircraft LLC Models 690, 690A, and 690B Airplanes

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

2008-13-30

final rule

Airworthiness Directives; Gulfstream Aerospace LP Model Astra SPX, 1125 Westwind Astra, and Gulfstream 100 Airplanes

Unsafe Condition: Two of the fasteners used to attach the 'scissors' to the horizontal and vertical stabilizers were found broken during routine maintenance. Failure of these attachment fasteners could result in pos...

Effective: Aug 12, 2008 Category: aircraft Compliance: Within 30 days after the effective date of this AD for AFM revision; within 25 flight hours or 30...

Why matched: Airworthiness Directives; Gulfstream Aerospace LP Model Astra SPX, 1125 Westwind Astra, and Gulfstream 100 Airplanes

2008-14-11

final rule

Airworthiness Directives; Boeing Model 777-200, -200LR, -300, and -300ER Series Airplanes Approved for Extended-Range Twin-Engine Operational Performance Standards (ETOPS)

Unsafe Condition: The filter/regulator installed in the cargo fire suppression system did not meter the Halon for the certified duration during ETOPS flight tests.

Effective: Jul 23, 2008 Category: engine Compliance: Within 30 days after the effective date of this AD.

Why matched: Airworthiness Directives; Boeing Model 777-200, -200LR, -300, and -300ER Series Airplanes Approved for Extended-Range Twin-Engine Operational Performance Standards (ETOPS)

2006-16-18 R1

final rule

Airworthiness Directives; Sandel Avionics Incorporated Model ST3400 Terrain Awareness Warning System/Radio Magnetic Indicator (TAWS/ RMI) Units Approved Under Technical Standard Order(s) C113, C151a, or C151b; Installed on Various Small and Transport Category Airplanes

Unsafe Condition: A bearing error in the Sandel Avionics Incorporated Model ST3400 TAWS/RMI unit configured to receive bearing information from a VOR receiver interface via a composite video signal, due to a combina...

Effective: Jul 18, 2008 Category: appliance Compliance: Effective July 18, 2008

Why matched: Airworthiness Directives; Sandel Avionics Incorporated Model ST3400 Terrain Awareness Warning System/Radio Magnetic Indicator (TAWS/ RMI) Units Approved Under Technical Standard Order(s) C113, C151a, or C151b; Installed on Various Small and Transport Category Airplanes

2007-03-05

final rule

Airworthiness Directives; Gulfstream Aerospace LP Model Gulfstream 100 Airplanes, and Model Astra SPX and 1125 Westwind Astra Airplanes

Unsafe Condition: Incomplete closure of the main entry door, which may result in the door opening in flight, causing damage to wing, fuselage, engine, and/or tail, and possible damage to the airplane.

Effective: Feb 15, 2007 Category: engine Compliance: Before further flight

Why matched: Airworthiness Directives; Gulfstream Aerospace LP Model Gulfstream 100 Airplanes, and Model Astra SPX and 1125 Westwind Astra Airplanes

2006-15-01

final rule

Airworthiness Directives; Twin Commander Aircraft Corporation Models 690, 690A, and 690B Airplanes

Unsafe Condition: Cracks in the support structures for the inboard and center aileron hinge fittings on both wings, which could result in aileron failure.

Effective: Aug 21, 2006 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Twin Commander Aircraft Corporation Models 690, 690A, and 690B Airplanes

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

2006-08-01 Recurring

final rule

Airworthiness Directives; BURKHART GROB LUFT-UND-RAUMFAHRT GmbH & Co. KG, Model G 103 C Twin III SL Sailplanes

Unsafe Condition: Increased play of the propeller bearing and upper pulley wheel.

Effective: May 9, 2006 Category: propeller Compliance: Within 25 engine operating hours after May 9, 2006.

Why matched: Airworthiness Directives; BURKHART GROB LUFT-UND-RAUMFAHRT GmbH & Co. KG, Model G 103 C Twin III SL Sailplanes

2006-01-01

final rule

Airworthiness Directives; Gulfstream Aerospace LP Model Gulfstream 100 Airplanes; and Model Astra SPX, and 1125 Westwind Astra Airplanes

Unsafe Condition: Failure of the steering brackets of the nose wheel steering assembly of the landing gear, and in one incident, loss of steering control.

Effective: Feb 16, 2006 Category: aircraft Compliance: Within 50 flight hours or 25 landings after the effective date of this AD, whichever is first.

Why matched: Airworthiness Directives; Gulfstream Aerospace LP Model Gulfstream 100 Airplanes; and Model Astra SPX, and 1125 Westwind Astra Airplanes

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

2005-26-14

final rule

Airworthiness Directives; BURKHARDT GROB LUFT-UND RAUMFA HRT GmbH & CO KG Model G103 TWIN ASTIR Sailplanes

Unsafe Condition: Cracks in the elevator lever, part number 103-3521, could cause the elevator lever to fail, resulting in loss of control of the sailplane.

Effective: Feb 6, 2006 Category: aircraft Compliance: Within the next 25 hours time-in-service after February 6, 2006.

Why matched: Airworthiness Directives; BURKHARDT GROB LUFT-UND RAUMFAHRT GmbH & CO KG Model G103 TWIN ASTIR Sailplanes

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

2005-26-12

final rule

Airworthiness Directives; BURKHARDT GROB LUFT-UND RAUMFAHRT GmbH & CO KG Models G103 TWIN ASTIR, G103 TWIN II, G103A TWIN II ACRO, G103C TWIN III ACRO, and G 103 C Twin III SL Sailplanes

Unsafe Condition: Cracked center of gravity (CG) release hook attachment brackets could lead to abnormal or uncontrolled sailplane release, resulting in reduced or loss of sailplane control.

Effective: Feb 6, 2006 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; BURKHARDT GROB LUFT-UND RAUMFAHRT GmbH & CO KG Models G103 TWIN ASTIR, G103 TWIN II, G103A TWIN II ACRO, G103C TWIN III ACRO, and G 103 C Twin III SL Sailplanes

2003-19-14 R2

final rule

Airworthiness Directives; BURKHART GROB LUFT--UND RAUMFAHRT GmbH & CO KG Models G103 TWIN ASTIR, G103A TWIN II ACRO, and G103C TWIN III ACRO Sailplanes

Unsafe Condition: Damage to the fuselage during limit load flight could result in reduced structural integrity and loss of control of the sailplane.

Effective: Nov 30, 2005 Category: aircraft Compliance: before November 30, 2005

Why matched: Airworthiness Directives; BURKHART GROB LUFT--UND RAUMFAHRT GmbH & CO KG Models G103 TWIN ASTIR, G103A TWIN II ACRO, and G103C TWIN III ACRO Sailplanes

Amdt-39-14322

final rule

Airworthiness Directives; BURKHART GROB LUFT-UND RAUMFAHRT GmbH & CO KG Models G103 TWIN ASTIR, G103A TWIN II ACRO, and G103C TWIN III ACRO Sailplanes

Unsafe Condition: Damage to the fuselage during limit load flight, which could result in reduced structural integrity and lead to loss of control of the sailplane.

Effective: Nov 30, 2005 Category: aircraft Compliance: Within 12 months of the effective date (November 30, 2005).

2005-18-20

final rule

Airworthiness Directives; Goodrich De-icing and Specialty Systems “FASTprop” Propeller De-icers

Unsafe Condition: Goodrich De-icing and Specialty Systems 'FASTprop' propeller de-icers becoming loose or debonded, and detaching from propeller blades during operation.

Effective: Oct 14, 2005 Category: propeller Compliance: Before further flight

Why matched: Airworthiness Directives; Goodrich De-icing and Specialty Systems "FASTprop" Propeller De-icers

Technical illustration of an aircraft propeller assembly
Problem area Propeller

2005-01-19

final rule

Airworthiness Directives; GARMIN International Inc. GTX 33, GTX 33D, GTX 330, and GTX 330D Mode S Transponders

Unsafe Condition: The GTX 33/33D/330/330D Mode S transponders may detect the S1 (suppression) interrogating pulse below the minimum trigger level (MTL) and, in some circumstances, not reply. This could lead to inacc...

Effective: Feb 23, 2005 Category: aircraft Compliance: Within 12 months of the effective date (February 23, 2005).

Why matched: Airworthiness Directives; GARMIN International Inc. GTX 33, GTX 33D, GTX 330, and GTX 330D Mode S Transponders

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