Document ID: chunk:federal_register_of_legislation:F2006B01957:body:0
Version: federal_register_of_legislation:F2006B01957
Segment Type: other
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Character Range: 0–1674

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Airbus Industrie A319, A320 and A321 Series Aeroplanes

 AD/A320/69
 Amdt 2

     Passenger Door and Emergency Door Actuator Striker Mechanism

 7/99

            Applicability: All Airbus Industrie A319, A320, and A321 aircraft, without Airbus Industrie modification 26015 (doors 1 and 4 for A319, A320, and A321 aircraft) and Airbus Industrie modification 26211 (doors 2 and 3 for the A321 aircraft) or Airbus Industrie Service Bulletin (SB) A320-52-1094 Revision 1, incorporated.

Requirement: Inspect in accordance with the requirements of DGAC AD 1998-482-122(B) R1.

            Note: Airbus Industrie A320 AOT 52-12R1 and SB A320-52-1094 and SB A320-52- 1094R1 refer.

            Compliance: Initial and repetitive inspections as specified in the Requirement Document with a revised effective date of 25 March 1999.

            The compliance time of this Directive remains unchanged. This Amendment becomes effective on 15 July 1999.
            Background: This Directive requires certain actions to prevent jamming of the passenger door and emergency door actuator mechanism that could delay the evacuation of passengers during an emergency.

            Amendment 1 introduced additional requirements.

            Amendment 2 is issued in response to a new DGAC AD which deletes reference to a certain applicability modification.

            Amendment 1 of this Airworthiness Directive became effective on 25 March 1999. The original issue of this Airworthiness Directive became effective on 18 July 1996.