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2024-14-03

final rule

Airworthiness Directives; Various Airplanes

Unsafe Condition: an un-commanded automatic pitch trim runaway when the autopilot was first engaged, which could result in un-commanded automatic pitch trim runaway and loss of control of the airplane.

Effective: Aug 20, 2024 Category: aircraft Compliance: Within 12 months after the effective date of this AD

Why matched: Airworthiness Directives; Various Airplanes

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

2012-02-10 Recurring

final rule

Airworthiness Directives; CPAC, Inc. Airplanes

Unsafe Condition: Cracks in the elevator spar, which could lead to structural failure of the elevator spar.

Effective: Mar 15, 2012 Category: aircraft Compliance: Within 12 months of the effective date (March 15, 2012).

Why matched: Airworthiness Directives; CPAC, Inc. Airplanes

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

2011-07-13

final rule

Airworthiness Directives; CPAC, Inc. (Type Certificate Formerly Held by Commander Aircraft Corporation, Gulfstream Aerospace Corporation, and Rockwell International) Models 112, 112B, 112TC, 112TCA, 114, 114A, 114B, and 114TC Airplanes

Unsafe Condition: Cracking of the elevator spar, which could lead to structural failure and separation of the elevator from the airplane, resulting in loss of control.

Effective: Apr 4, 2011 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; CPAC, Inc. (Type Certificate Formerly Held by Commander Aircraft Corporation, Gulfstream Aerospace Corporation, and Rockwell International) Models 112, 112B, 112TC, 112TCA, 114, 114A, 114B, and 114TC Airplanes

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

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

2006-12-07

final rule

Airworthiness Directives; Engine Components Inc. (ECi) Reciprocating Engine Cylinder Assemblies

Unsafe Condition: Cracks in the cylinder assemblies and possible engine failure caused by separation of a cylinder head.

Effective: Jul 11, 2006 Category: engine Compliance: Before further flight

Why matched: Airworthiness Directives; Engine Components Inc. (ECi) Reciprocating Engine Cylinder Assemblies

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

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

2000-11-04

final rule

Airworthiness Directives; Commander Aircraft Company Model 114TC Airplanes

Unsafe Condition: Failure of the Aeroquip V-band exhaust clamp (Aeroquip part number 00624-55677-340M or Lycoming alternate part number 40D21162-340M), which attaches the exhaust stack to the turbocharger, could res...

Effective: Jun 23, 2000 Category: aircraft Compliance: Within 25 hours time-in-service after June 23, 2000

Why matched: Airworthiness Directives; Commander Aircraft Company Model 114TC Airplanes

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

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

Amdt-39-11548

final rule

Airworthiness Directives; Twin Commander Aircraft Corporation 600 Series Airplanes

Unsafe Condition: Reports of in-flight incidents and an accident in icing conditions where the airframe pneumatic deicing boots were not activated, leading to reduced controllability due to ice accumulation.

Effective: Mar 24, 2000 Category: aircraft Compliance: Not specified in the source.

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

Amdt-39-10821

final rule

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

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

Effective: Jan 5, 1999 Category: aircraft Compliance: Within the compliance time specified in AD 98-08-25, as per Twin Commander Service Bulletin 224, ...

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

98-08-25 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

Amdt-39-10801

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: Operating in severe icing conditions without clear procedures and limitations may lead to reduced aircraft control and potential structural failure due to ice accumulation.

Effective: Nov 3, 1998 Category: aircraft Compliance: Before further flight

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

98-20-34

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.

98-07-17

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

Amdt-39-10437

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 due to worn and frayed cables attributed to flap pulley grooves that are too narrow.

Effective: May 29, 1998 Category: aircraft Compliance: Before further flight

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

Amdt-39-10468 Recurring

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.

Effective: May 18, 1998 Category: aircraft Compliance: Before further flight

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

Amdt-39-10474

final rule

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

Unsafe Condition: Collapse of the nose landing gear (NLG) caused by a failed drag link bolt due to defective manufacture of a certain lot of bolts used in the NLG.

Effective: May 18, 1998 Category: aircraft Compliance: Before further flight

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

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 :

94-04-15

final rule

Airworthiness Directives: Twin Commander Aircraft Corporation Models 500, 560A, 560E, 680, 680E, and 720 Airplanes

Unsafe Condition: Failure of the wing structure caused by a cracked wing front spar lower cap at Wing Station (WS) 96 due to interference, fretting, or corrosion between the firewall flange and spar cap flange.

Effective: Apr 12, 1994 Category: aircraft Compliance: within the next 50 hours time-in-service after the effective date of this AD

Why matched: Airworthiness Directives: Twin Commander Aircraft Corporation Models 500, 560A, 560E, 680, 680E, and 720 Airplanes

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

94-04-13

final rule

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

Unsafe Condition: Failure of the wing structure caused by cracks in the lower front spar cap.

Effective: Apr 12, 1994 Category: aircraft Compliance: Initially within the next 50 hours time-in-service (TIS), or 500 hours after spar cap replacement...

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