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7 results found (2113ms)

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2007-23-06

final rule

Airworthiness Directives; CTRM Aviation Sdn. Bhd. (Formerly Eagle Aircraft (Malaysia) Sdn. Bhd.) Model Eagle 150B Airplanes

Unsafe Condition: Severe exfoliation corrosion on Wing/Canard Flap Hinges, P/N 5731D01-16 (middle and outboard hinges), leading to a 50% reduction in thickness. Corrosion is not easily detected due to the hinge's po...

Effective: Dec 11, 2007 Category: aircraft Compliance: Within 25 hours time-in-service (TIS) after December 11, 2007

Why matched: Airworthiness Directives; CTRM Aviation Sdn. Bhd. (Formerly Eagle Aircraft (Malaysia) Sdn. Bhd.) Model Eagle 150B Airplanes

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2007-04-02 Recurring

final rule

Airworthiness Directives; CTRM Aviation Sdn. Bhd. (Formerly Eagle Aircraft (Malaysia) Sdn. Bhd.) Model Eagle 150B Airplanes

Unsafe Condition: Cracks in the canard inboard flap hinge support brackets could result in loss of retention of controls and consequently, loss of airplane control.

Effective: Mar 21, 2007 Category: aircraft Compliance: Before further flight for initial inspection; repetitively before the first flight of each day fo...

Why matched: Airworthiness Directives; CTRM Aviation Sdn. Bhd. (Formerly Eagle Aircraft (Malaysia) Sdn. Bhd.) Model Eagle 150B Airplanes

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2005-05-14

final rule

Airworthiness Directives; Eagle Aircraft (Malaysia) Sdn. Bhd. Model Eagle 150B Airplanes

Unsafe Condition: Binding of the co-pilot rudder pedal assembly due to premature wear of the bushing, which could result in loss of co-pilot rudder and brake control.

Effective: Apr 22, 2005 Category: aircraft Compliance: Inspect within 30 days after April 22, 2005 (the effective date of this AD).

Why matched: Airworthiness Directives; Eagle Aircraft (Malaysia) Sdn. Bhd. Model Eagle 150B Airplanes

Technical illustration of an aircraft flight control surface and actuator
Problem area Flight controls
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2004-26-01

final rule

Airworthiness Directives; Eagle Aircraft (Malaysia) Sdn. Bhd. Model Eagle 150B Airplanes

Unsafe Condition: Unwelded areas on the undercarriage attach bracket could result in cracks, leading to loss of control of the airplane.

Effective: Jan 31, 2005 Category: aircraft Compliance: Within 50 hours time-in-service after January 31, 2005

Why matched: Airworthiness Directives; Eagle Aircraft (Malaysia) Sdn. Bhd. Model Eagle 150B Airplanes

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2003-19-07

final rule

Airworthiness Directives; Eagle Aircraft (Malaysia) Sdn. Bhd. Model 150B Airplanes

Unsafe Condition: Detachment of the rear spar bracket from the canard rear spar, which could result in failure of the canard rear spar.

Effective: Nov 3, 2003 Category: aircraft Compliance: Within the next 100 hours time-in-service after November 3, 2003, unless already accomplished.

Why matched: Airworthiness Directives; Eagle Aircraft (Malaysia) Sdn. Bhd. Model 150B Airplanes

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2002-02-01

final rule

Airworthiness Directives; Eagle Aircraft Pty. Ltd. Model 150B Airplanes

Unsafe Condition: Failure of the throttle control assembly caused by rivets of the wrong size.

Effective: Mar 21, 2002 Category: aircraft Compliance: Before further flight.

Why matched: Airworthiness Directives; Eagle Aircraft Pty. Ltd. Model 150B Airplanes

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2001-09-16

final rule

Airworthiness Directives; Eagle Aircraft Pty. Ltd. Model 150B Airplanes

Unsafe Condition: Fraying and broken strands of rudder cables caused by chafing against the rudder cable pulleys.

Effective: Jun 29, 2001 Category: aircraft Compliance: Within the next 100 hours time-in-service (TIS) after the effective date of this AD for inspectio...

Why matched: Airworthiness Directives; Eagle Aircraft Pty. Ltd. Model 150B Airplanes

Technical illustration of an aircraft flight control surface and actuator
Problem area Flight controls
View Details View AD (PDF) ↗