Document ID: chunk:federal_register_of_legislation:F2006B01937:body:0
Version: federal_register_of_legislation:F2006B01937
Segment Type: other
Provision Reference: 
Character Range: 0–1479

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/A320/47
 Amdt 2

        Fuselage - Pressure Floor Between Frames 42 and 43

 6/96

            Applicability: Serial Numbers 002 to 008, 010 to 014, 016 to 078, 080 to 104, and 106 and 107, without Airbus Industrie SB A320-53-1023 Rev.7 incorporated.

 Requirement: Action in accordance with Airbus Industrie SB A320-53-1024 Rev. 2.

            Note 1. DGAC AD 92-205-033(B)R2 refers.

            Note 2. For aircraft with Airbus Industrie SB A320-53-1025 Rev. 6 or earlier Revisions incorporated, refer to AD/A320/67.

            Compliance: Prior to attaining 12 000 flights; thereafter at the intervals specified in the Requirement Document until modified, and this amendment is effective from 23 May 1996.

            Background: During the full scale fatigue test, cracking was experienced in the outer floor beams, box beams, and other associated structure.

            Amendment 1 provides relief for operators that have already incorporated SB A320-53-1023 at issues before Revision 3.

            Amendment 2 amends the applicability and provides terminating action through Airbus Industrie SB A320-53-1023 Rev. 7.

            The original issue of this AD became effective on 27 April 1995. Amendment 1 of this AD became effective on 20 July 1995.