I AM THE LAW
Browse › Legislation › Commonwealth

AD/A320/142 - Trust Reverser - Piston Rod Chrome Plating

Legislation · Commonwealth · 2004
Airworthiness Directive - AD/A320/142 - Trust Reverser - Piston Rod Chrome Plating Airworthiness Directive - AD/A320/142 - Trust Reverser - Piston Rod Chrome Plating CASA Airworthiness Directive Jurisdiction:Commonwealth of Australia;CorporateName:Civil Aviation Safety Authority; Issue 11/2002,Aircraft above 5700 kg,Airbus Industrie A319, A320 and A321 Series Aeroplanes,Trust Reverser - Piston Rod Chrome Plating,142 DellaCa, Donna 2 1 2022-10-26T04:49:00Z 2022-10-26T04:50:00Z 1 258 1477 Office of Parliamentary Counsel 12 3 1732 16.0000 2006-09-22T00:00:00Z Toolkit http://www.activepdf.com 2022-10-26T00:00:00Z COMMONWEALTH OF AUSTRALIA   (Civil Aviation Regulations 1998) , PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY SCHEDULE OF AIRWORTHINESS DIRECTIVES   AIRWORTHINESS DIRECTIVE For the reasons set out in the background section, the CASA delegate whose signature appears below issues the following Airworthiness Directive (AD) under subregulation 39.1 (1) of CAR 1998. The AD requires that the action set out in the requirement section (being action that the delegate considers necessary to correct the unsafe condition) be taken in relation to the aircraft or aeronautical product mentioned in the applicability section: (a) in the circumstances mentioned in the requirement section; and (b) in accordance with the instructions set out in the requirement section; and (c) at the time mentioned in the compliance section.   Airbus Industrie A319, A320 and A321 Series Aeroplanes   AD/A320/142   Trust Reverser - Piston Rod Chrome Plating   11/2002   Applicability:   All A319, A320 and A321 series aeroplanes as identified in the requirement document.   Requirement:   Action per DGAC AD 2002- 337(B)R1.   Note: DGAC AD 2002-337(B) R1 refers.   Compliance:   Per the requirement document with a revised effective date of 31 October 2002.   This Airworthiness Directive becomes effective on 31 October 2002.   Background:   Error during the repair and rigging of thrust reverser blocker door actuators has resulted in a situation of potential door deployment in- flight. This directive mandates the replacement of affected actuators.   James Coyne Delegate of the Civil Aviation Safety Authority 24 September 2002                               The above AD is notified in the Commonwealth of Australia Gazette on 9 October 2002.       Page 1 of 1