Lancair Airworthiness Directives

7 ADs indexed for Lancair aircraft.

Models

Recent ADs

2011-03-04 Recurring

final rule

Airworthiness Directives; Cessna Aircraft Company (Type Certificate Previously Held by Columbia Aircraft Manufacturing (Previously the Lancair Company)) Models LC40-550FG, LC41-550FG, and LC42-550FG Airplanes

Unsafe Condition: Damage in the rudder hinges and the rudder hinge brackets, which could result in failure of the rudder. This failure could lead to loss of control.

Effective: Mar 14, 2011 Category: aircraft Compliance: Within 50 flight hours after the effective date of this AD.

Why matched: Airworthiness Directives; Cessna Aircraft Company (Type Certificate Previously Held by Columbia Aircraft Manufacturing (Previously the Lancair Company)) Models LC40-550FG, LC41-550FG, and LC42-550FG Airplanes

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

2010-26-54

final rule

Airworthiness Directives; Cessna Aircraft Company (Cessna) (Type Certificate A00003SE Previously Held by Columbia Aircraft Manufacturing (Previously The Lancair Company)) Models LC41-550FG and LC42-550FG Airplanes

Unsafe Condition: Disbonding of the wing skin from the upper forward wing spar, as occurred in a Cessna Model LC41-550FG airplane during a production acceptance flight test, leading to a significant structural failure.

Effective: Jan 10, 2011 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Cessna Aircraft Company (Cessna) (Type Certificate A00003SE Previously Held by Columbia Aircraft Manufacturing (Previously The Lancair Company)) Models LC41-550FG and LC42-550FG Airplanes

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

2009-09-09 Recurring

final rule

Airworthiness Directives; Cessna Aircraft Company (Type Certificate Previously Held by Columbia Aircraft Manufacturing (Previously The Lancair Company)) Models LC40-550FG, LC41-550FG, and LC42-550FG Airplanes

Unsafe Condition: Corrosion of the anodized 2024 aluminum rudder hinge brackets, leading to cracking, deformation, and discoloration, which could result in failure of the rudder and loss of control.

Effective: May 11, 2009 Category: aircraft Compliance: Within 50 flight hours after the effective date of this AD.

Why matched: Airworthiness Directives; Cessna Aircraft Company (Type Certificate Previously Held by Columbia Aircraft Manufacturing (Previously The Lancair Company)) Models LC40-550FG, LC41-550FG, and LC42-550FG Airplanes

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

2007-07-06 Recurring

final rule

Airworthiness Directives; Columbia Aircraft Manufacturing (Previously the Lancair Company) Models LC40-550FG, LC41-550FG, and LC42-550FG Airplanes

Unsafe Condition: Possible foreign object contamination of the aileron and elevator linear bearings could result in jamming of the control systems, leading to failure and loss of control.

Effective: Apr 9, 2007 Category: aircraft Compliance: Before further flight.

Why matched: Airworthiness Directives; Columbia Aircraft Manufacturing (Previously the Lancair Company) Models LC40-550FG, LC41-550FG, and LC42-550FG Airplanes

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

2005-12-20

final rule

Airworthiness Directives; The Lancair Company Model LC41-550FG Airplanes

Unsafe Condition: Cracks in the elevator torque tube assembly could lead to structural failure of the assembly.

Effective: Jun 21, 2005 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; The Lancair Company Model LC41-550FG Airplanes

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

2005-02-01

final rule

Airworthiness Directives; The Lancair Company Models LC40-550FG and LC42-550FG Airplanes

Unsafe Condition: Flight testing revealed that the takeoff distance values for the affected airplanes could not be duplicated, predicting distances as much as 65 percent below actual requirements.

Effective: Jan 21, 2005 Category: aircraft Compliance: Before further flight after January 21, 2005

Why matched: Airworthiness Directives; The Lancair Company Models LC40-550FG and LC42-550FG Airplanes

2004-06-09 Recurring

final rule

Airworthiness Directives; The Lancair Company Models LC40-550FG and LC42-550FG Airplanes

Unsafe Condition: Fuel pressure transducer wearing through at the threads where it attaches to the fuel line, potentially leading to failure of the transducer threaded fitting and resulting fuel leaks.

Effective: May 3, 2004 Category: engine Compliance: Within 50 flight hours after the effective date of the AD.

Why matched: Airworthiness Directives; The Lancair Company Models LC40-550FG and LC42-550FG Airplanes

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

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