Twin Commander Aircraft LLC Airworthiness Directives

59 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 680-T 7 ADs 695B 7 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 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

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

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

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

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

2003-07-03 Recurring

final rule

Airworthiness Directives; Twin Commander Aircraft Corporation Models 690D, 695A, and 695B Airplanes

Unsafe Condition: Fatigue damage in the wing and fuselage structure could result in structural failure and loss of control of the airplane.

Effective: May 16, 2003 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Twin Commander Aircraft Corporation Models 690D, 695A, and 695B Airplanes

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

2000-02-30

final rule

Airworthiness Directives; Twin Commander Aircraft Corporation 600 Series Airplanes

Unsafe Condition: The information necessary to activate the pneumatic wing and tail deicing boots at the first signs of ice accumulation is critical for flight in icing conditions. If not addressed, flight crews cou...

Effective: Mar 24, 2000 Category: aircraft Compliance: Within 10 calendar days after the effective date (March 24, 2000)

Why matched: Airworthiness Directives; Twin Commander Aircraft Corporation 600 Series Airplanes

98-08-25 R1

final rule

Airworthiness Directives; Twin Commander Aircraft Corporation 500, 680, 690, and 695 Series Airplanes

Unsafe Condition: Failure of a nose landing gear (NLG) drag link bolt could result in NLG collapse and loss of control during landing operations.

Effective: Jan 5, 1999 Category: aircraft Compliance: Effective January 5, 1999.

Why matched: Airworthiness Directives; Twin Commander Aircraft Corporation 500, 680, 690, and 695 Series Airplanes

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

98-20-34

final rule

Airworthiness Directives; Twin Commander Aircraft Corporation Models 500, 500-A, 500-B, 500-S, 500-U, 520, 560, 560-A, 560-E, 560-F, 680, 680-E, 680FL(P), 680T, 680V, 680W, 681, 685, 690, 690A, 690B, 690C, 690D, 695, 695A, 695B, and 720 Airplanes.

Unsafe Condition: Airplane Flight Manuals--Severe Icing Conditions

Effective: Nov 3, 1998 Category: aircraft

Why matched: Airworthiness Directives; Twin Commander Aircraft Corporation Models 500, 500-A, 500-B, 500-S, 500-U, 520, 560, 560-A, 560-E, 560-F, 680, 680-E, 680FL(P), 680T, 680V, 680W, 681, 685, 690, 690A, 690B, 690C, 690D, 695, 695A, 695B, and 720 Airplanes.

98-14-03

final rule

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

Unsafe Condition: The inability of AlliedSignal Inc. KT 76A ATC transponders to coordinate with ground-based ATC radar sites and nearby TCAS-equipped aircraft, caused by silver migration in resistor network modules ...

Effective: Aug 16, 1998 Category: appliance Compliance: within 12 calendar months

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

98-07-17

final rule

Airworthiness Directives; Twin Commander Aircraft Corporation 500, 520, 560, 680, 681, 685, 690, 695, and 720 Series Airplanes

Unsafe Condition: Failure of a flap system cable caused by fatigue, which could result in loss of control of the airplane.

Effective: May 29, 1998 Category: aircraft Compliance: Within the next 300 hours time-in-service (TIS) after the effective date of this AD

Why matched: Airworthiness Directives; Twin Commander Aircraft Corporation 500, 520, 560, 680, 681, 685, 690, 695, and 720 Series Airplanes

98-08-19

final rule

Airworthiness Directives; Twin Commander Aircraft Corporation 500, 600, and 700 Series Airplanes

Unsafe Condition: Cracks in the wing to fuselage attachment brackets and straps at wing station 24 and fuselage frames could cause structural failure and loss of control of the airplane.

Effective: May 18, 1998 Category: aircraft Compliance: Prior to further flight if cracks are found. Inspections must be repeated at regular intervals un...

Why matched: Airworthiness Directives; Twin Commander Aircraft Corporation 500, 600, and 700 Series Airplanes

96-12-22

final rule

Airworthiness Directives; Cessna Aircraft Company Engine Oil Filter Adapter Assemblies Installed on Aircraft

Unsafe Condition: Loose or separated engine oil filter adapters could cause loss of engine oil, leading to engine stoppage while in flight and loss of control of the airplane.

Effective: Jul 31, 1996 Category: appliance Compliance: Within the next 100 hours time-in-service (TIS) after the effective date or when the engine oil f...

Why matched: Airworthiness Directives; Cessna Aircraft Company Engine Oil Filter Adapter Assemblies Installed on Aircraft

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

95-19-18

final rule

Airworthiness Directives; Twin Commander Aircraft Corporation Models 680T and 680V, 680W, 681, 690, 690A, 690B, 690C, 690D, 695, 695A, 695B Airplanes

Unsafe Condition: Structural damage to the airplane caused by excessive turbulence, which could result in loss of the airplane.

Effective: Oct 25, 1995 Category: aircraft Compliance: within the next 50 hours time-in-service after the effective date of this AD, unless already acco...

Why matched: Airworthiness Directives; Twin Commander Aircraft Corporation Models 680T and 680V, 680W, 681, 690, 690A, 690B, 690C, 690D, 695, 695A, 695B Airplanes

95-12-23

final rule

Airworthiness Directives; Twin Commander Aircraft Corporation Models 690C and 695 Airplanes

Unsafe Condition: Wing damage caused by fatigue cracking, which could progress to structural failure if not detected and corrected.

Effective: Jul 30, 1995 Category: aircraft Compliance: Required upon the accumulation of 6,000 hours time-in-service (TIS) or within the next 50 hours T...

Why matched: Airworthiness Directives; Twin Commander Aircraft Corporation Models 690C and 695 Airplanes

95-13-02

final rule

Airworthiness Directives; Twin Commander Aircraft Corporation Models 685, 690, 690A, 690B, 690C, 690D, 695, 695A Airplanes :

Unsafe Condition: Failure of the vertical stabilizer as a result of cracks, which could result in loss of control of the airplane.

Effective: Jul 22, 1995 Category: aircraft Compliance: Required upon the accumulation of 2,000 hours time-in-service (TIS) on a vertical stabilizer or w...

Why matched: Airworthiness Directives; Twin Commander Aircraft Corporation Models 685, 690, 690A, 690B, 690C, 690D, 695, 695A Airplanes :

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