Document ID: chunk:federal_register_of_legislation:F2006B01967:body:0
Version: federal_register_of_legislation:F2006B01967
Segment Type: other
Provision Reference: 
Character Range: 0–1274

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/A320/78 Spoiler Phased Lift Dumping 2/97

 Applicability: All model A320-111, A320-211 A320-212, A320-231, A320-232, A321-111,
            A321-112 and A321-131 without Airbus Industrie modification 24745 or Airbus Industrie Service Bulletins A320-27-1088 dated 16 January 1995, Revision 1 dated 16
            May 1995 or Revision 2 dated 11 September 1995 incorporated.

            Requirement: Unless previously accomplished, modify the aeroplane in accordance with Airbus Industrie Service Bulletins A320-27-1088 dated 16 January 1995, Revision 1 dated 16 May 1995 or Revision 2 dated 11 September 1995 to activate the "phased lift dumping" function of the spoiler elevator computer.

            Note: DGAC AD 96-169-081(B) refers.

 Compliance: Prior to 30 September 1997.

            This Airworthiness Directive becomes effective on 30 January 1997.

            Background:  This Directive mandates measures designed to reduce the delay in activation of automatic deceleration means during landing with strong cross winds and/or on contaminated runways.