Airbus A319, A320 and A321 Series Aeroplanes

<table cellspacing="0" cellpadding="0" style="width:510.3pt; margin-top:0pt; margin-bottom:0pt; border-collapse:collapse"><tbody><tr><td style="width:74.35pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>Applicability:</span></p></td><td style="width:414.55pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>A319, A320 and A321 series aeroplanes manufactured prior to 1 January 2002.</span></p></td></tr><tr><td style="width:74.35pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>Requirement:</span></p></td><td style="width:414.55pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><ol style="margin:0pt; padding-left:0pt"><li class="ListParagraph" style="margin-left:14.05pt; margin-bottom:0pt; padding-left:14.35pt"><span>Determine the applicability of </span><span>the </span><span>French Directorate General for Civil Aviation </span><span style="font-weight:bold">(</span><span style="font-weight:bold; font-style:italic">DGAC</span><span style="font-weight:bold">)</span><span> and United States of America Federal Aviation Administration </span><span style="font-weight:bold">(</span><span style="font-weight:bold; font-style:italic">FAA</span><span style="font-weight:bold">)</span><span> </span><span>Airworthiness Directives (AD) listed in Table 1</span><span>, as in force from time to time</span><span>.</span></li></ol><p><span style="font-style:italic">Note 1:</span><span style="font-style:italic"> </span><span style="font-style:italic">The words “as in force from time to time” require compliance with the most</span><span style="font-style:italic"> </span><span style="font-style:italic">recent version of the referenced document.</span></p><p class="ListParagraph" style="margin-left:28.85pt; margin-bottom:0pt; text-indent:-28.85pt"><span><span>2.</span></span><span style="font:7pt 'Times New Roman'"> </span><span>If it is determined that a</span><span>n </span><span>AD</span><span> </span><span>listed in Table 1 is applicable and has not</span><span> </span><span>been previously accomplished, perform the actions required by that AD.</span></p><p style="margin-bottom:0pt; text-align:center"><span style="font-weight:bold">Table 1</span></p><table cellspacing="0" cellpadding="0" style="margin-top:0pt; margin-bottom:0pt; border:0.75pt solid #000000; border-collapse:collapse"><tbody><tr><td style="width:127.1pt; border-right:0.75pt solid #000000; border-bottom:0.75pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top"><p class="Note" style="text-align:center"><span style="font-weight:bold; font-style:normal">AD Number</span></p></td><td style="width:127.15pt; border-right:0.75pt solid #000000; border-left:0.75pt solid #000000; border-bottom:0.75pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top"><p class="Note" style="text-align:center"><span style="font-weight:bold; font-style:normal">Effective Date</span></p></td><td style="width:127.15pt; border-left:0.75pt solid #000000; border-bottom:0.75pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top"><p class="Note" style="text-align:center"><span style="font-weight:bold; font-style:normal">Title</span></p></td></tr><tr><td style="width:127.1pt; border-top:0.75pt solid #000000; border-right:0.75pt solid #000000; border-bottom:0.75pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top"><p class="Note"><span style="font-style:normal">1992-164-026(B)</span></p></td><td style="width:127.15pt; border:0.75pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top"><p class="Note"><span style="font-style:normal">29 August 1992</span></p></td><td style="width:127.15pt; border-top:0.75pt solid #000000; border-left:0.75pt solid #000000; border-bottom:0.75pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top"><p class="Note"><span style="font-style:normal">Reinforcement of nose landing gear wheels</span></p></td></tr><tr><td style="width:127.1pt; border-top:0.75pt solid #000000; border-right:0.75pt solid #000000; border-bottom:0.75pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top"><p class="Note"><span style="font-style:normal">1</span><span style="font-style:normal">992-211-036(B) R1</span></p></td><td style="width:127.15pt; border:0.75pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top"><p class="Note"><span style="font-style:normal">9 May 1993</span></p></td><td style="width:127.15pt; border-top:0.75pt solid #000000; border-left:0.75pt solid #000000; border-bottom:0.75pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top"><p class="Note"><span style="font-style:normal">Trimmable horizontal stabilizer</span></p></td></tr><tr><td style="width:127.1pt; border-top:0.75pt solid #000000; border-right:0.75pt solid #000000; border-bottom:0.75pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top"><p class="Note"><span style="font-style:normal">1992-271-039(B) R3</span></p></td><td style="width:127.15pt; border:0.75pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top"><p class="Note"><span style="font-style:normal">23 March 1996</span></p></td><td style="width:127.15pt; border-top:0.75pt solid #000000; border-left:0.75pt solid #000000; border-bottom:0.75pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top"><p class="Note"><span style="font-style:normal">Electric terminal blocks</span></p></td></tr><tr><td style="width:127.1pt; border-top:0.75pt solid #000000; border-right:0.75pt solid #000000; border-bottom:0.75pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top"><p class="Note"><span style="font-style:normal">1994-030-050(B)</span></p><p class="Note"><span style="font-style:normal"></span></p></td><td style="width:127.15pt; border:0.75pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top"><p class="Note"><span style="font-style:normal">12 February1994</span></p></td><td style="width:127.15pt; border-top:0.75pt solid #000000; border-left:0.75pt solid #000000; border-bottom:0.75pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top"><p class="Note"><span style="font-style:normal">Junction box and electrical harness</span><span style="font-style:normal"> on CFM 56-5A</span></p></td></tr><tr><td style="width:127.1pt; border-top:0.75pt solid #000000; border-right:0.75pt solid #000000; border-bottom:0.75pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top"><p class="Note"><span style="font-style:normal">1994-058-053(B) R1</span></p></td><td style="width:127.15pt; border:0.75pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top"><p class="Note"><span style="font-style:normal">16 July 1994</span></p></td><td style="width:127.15pt; border-top:0.75pt solid #000000; border-left:0.75pt solid #000000; border-bottom:0.75pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top"><p class="Note"><span style="font-style:normal">IAE V2500-A1 engine fire extinguisher distribution pipe</span></p></td></tr><tr><td style="width:127.1pt; border-top:0.75pt solid #000000; border-right:0.75pt solid #000000; border-bottom:0.75pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top"><p class="Note"><span style="font-style:normal">1994-167-057(B)</span></p></td><td style="width:127.15pt; border:0.75pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top"><p class="Note"><span style="font-style:normal">30 July 1994</span></p></td><td style="width:127.15pt; border-top:0.75pt solid #000000; border-left:0.75pt solid #000000; border-bottom:0.75pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top"><p class="Note"><span style="font-style:normal">IAE V2500-A1 sealing of fire wall</span></p></td></tr><tr><td style="width:127.1pt; border-top:0.75pt solid #000000; border-right:0.75pt solid #000000; border-bottom:0.75pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top"><p class="Note"><span style="font-style:normal">1</span><span style="font-style:normal">995-016-063(B)</span></p></td><td style="width:127.15pt; border:0.75pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top"><p class="Note"><span style="font-style:normal">28 January 1995</span></p></td><td style="width:127.15pt; border-top:0.75pt solid #000000; border-left:0.75pt solid #000000; border-bottom:0.75pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top"><p class="Note"><span style="font-style:normal">Main landing gear shock absorber upper bearing dowel retention</span></p></td></tr><tr><td style="width:127.1pt; border-top:0.75pt solid #000000; border-right:0.75pt solid #000000; border-bottom:0.75pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top"><p class="Note"><span style="font-style:normal">1996-170-082(B)</span></p></td><td style="width:127.15pt; border:0.75pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top"><p class="Note"><span style="font-style:normal">7 September 1996</span></p></td><td style="width:127.15pt; border-top:0.75pt solid #000000; border-left:0.75pt solid #000000; border-bottom:0.75pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top"><p class="Note"><span style="font-style:normal">Fuel pump strainer</span></p></td></tr><tr><td style="width:127.1pt; border-top:0.75pt solid #000000; border-right:0.75pt solid #000000; border-bottom:0.75pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top"><p class="Note"><span style="font-style:normal">FAA AD 97-03-06</span></p></td><td style="width:127.15pt; border:0.75pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top"><p class="Note"><span style="font-style:normal">6 March 1997</span></p></td><td style="width:127.15pt; border-top:0.75pt solid #000000; border-left:0.75pt solid #000000; border-bottom:0.75pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top"><p class="Note"><span style="font-style:normal">Auxiliary Power International Corporation (APIC) Model APS3200 Auxiliary Power Units</span></p></td></tr><tr><td style="width:127.1pt; border-top:0.75pt solid #000000; border-right:0.75pt solid #000000; border-bottom:0.75pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top"><p><span>1997-203-102(B)R1</span></p><p class="Note"><span style="font-style:normal"></span></p></td><td style="width:127.15pt; border:0.75pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top"><p class="Note"><span style="font-style:normal">18 April 1998</span></p></td><td style="width:127.15pt; border-top:0.75pt solid #000000; border-left:0.75pt solid #000000; border-bottom:0.75pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top"><p class="Note"><span style="font-style:normal">Probe Heater Computer</span></p></td></tr><tr><td style="width:127.1pt; border-top:0.75pt solid #000000; border-right:0.75pt solid #000000; border-bottom:0.75pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top"><p><span>1998-152-114(B)</span></p></td><td style="width:127.15pt; border:0.75pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top"><p class="Note"><span style="font-style:normal">18 April 1998</span></p></td><td style="width:127.15pt; border-top:0.75pt solid #000000; border-left:0.75pt solid #000000; border-bottom:0.75pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top"><p><span>Probe Heater Computer (ATA 30)</span></p><p><span>Test Procedures</span></p></td></tr><tr><td style="width:127.1pt; border-top:0.75pt solid #000000; border-right:0.75pt solid #000000; border-bottom:0.75pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top"><p><span>1998-451-121(B)</span></p></td><td style="width:127.15pt; border:0.75pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top"><p class="Note"><span style="font-style:normal">28 November 1998</span></p></td><td style="width:127.15pt; border-top:0.75pt solid #000000; border-left:0.75pt solid #000000; border-bottom:0.75pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top"><p class="Note"><span style="font-style:normal">ILS Receiver (ATA 34)</span></p></td></tr><tr><td style="width:127.1pt; border-top:0.75pt solid #000000; border-right:0.75pt solid #000000; border-bottom:0.75pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top"><p><span>1999-361-138(B)</span></p></td><td style="width:127.15pt; border:0.75pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top"><p class="Note"><span style="font-style:normal">18 September 1999</span></p></td><td style="width:127.15pt; border-top:0.75pt solid #000000; border-left:0.75pt solid #000000; border-bottom:0.75pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top"><p class="Note"><span style="font-style:normal">Litton GPSSU (ATA 34)</span></p></td></tr><tr><td style="width:127.1pt; border-top:0.75pt solid #000000; border-right:0.75pt solid #000000; border-bottom:0.75pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top"><p><span>2000-004-142(B)</span></p></td><td style="width:127.15pt; border:0.75pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top"><p class="Note"><span style="font-style:normal">22 January 2000</span></p></td><td style="width:127.15pt; border-top:0.75pt solid #000000; border-left:0.75pt solid #000000; border-bottom:0.75pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top"><p><span>Rockwell Collins Radio Altimeter</span><span> </span><span>Software Anomalies (ATA 34)</span></p></td></tr><tr><td style="width:127.1pt; border-top:0.75pt solid #000000; border-right:0.75pt solid #000000; border-bottom:0.75pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top"><p><span>2001-271(B)</span></p></td><td style="width:127.15pt; border:0.75pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top"><p class="Note"><span style="font-style:normal">7 July 2001</span></p></td><td style="width:127.15pt; border-top:0.75pt solid #000000; border-left:0.75pt solid #000000; border-bottom:0.75pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top"><p><span>Loss of Fuel Quantity Indication</span><span> </span><span>on Centr</span><span>e</span><span> Tank (ATA 28)</span></p></td></tr><tr><td style="width:127.1pt; border-top:0.75pt solid #000000; border-right:0.75pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top"><p><span>2001-363(B)</span></p><p><span></span></p></td><td style="width:127.15pt; border-top:0.75pt solid #000000; border-right:0.75pt solid #000000; border-left:0.75pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top"><p class="Note"><span style="font-style:normal">18 August 2001</span></p></td><td style="width:127.15pt; border-top:0.75pt solid #000000; border-left:0.75pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top"><p><span>Oxygen Systems - Inspection of</span><span> </span><span>Oxygen Passenger Containers -</span><span style="font-style:italic">(</span><span style="font-style:italic">Dräeger</span><span style="font-style:italic"> Type I and II) (ATA 35)</span></p></td></tr></tbody></table><p class="Note"></p></td></tr><tr><td style="width:74.35pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>Compliance:</span></p></td><td style="width:414.55pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>If a certificate of airworthiness has not been issued for the aircraft - before issue of the</span><span> </span><span>certificate of airworthiness.</span></p><p><span>If a certificate of airworthiness has been issued for the aircraft - within 30 days after</span><span> </span><span>the effective date of this Directive.</span></p><p><span style="font-style:italic">Note </span><span style="font-style:italic">2</span><span style="font-style:italic">: </span><span style="font-style:italic"></span><span style="font-style:italic">Previous compliance with the requirements of DGAC AD 1996-293(B)R1 as required by CASA AD/APU/22, AD/A320/199 or AD/A320/199 </span><span style="font-style:italic">Amdt</span><span style="font-style:italic"> 1, constitutes compliance with</span><span style="font-style:italic"> FAA AD 97-03-06 as required</span><span style="font-style:italic"> </span><span style="font-style:italic">by </span><span style="font-style:italic">this amendment.</span></p><p><span>This </span><span>Airworthiness Directive commences</span><span> on </span><span>31</span><span> March 2</span><span>021</span><span>.</span></p></td></tr><tr><td style="width:74.35pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>Background:</span></p></td><td style="width:414.55pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>The ADs listed in Table </span><span>1 </span><span>of this Directive require one</span><span>-</span><span>time actions for which</span><span> </span><span>the compliance date and/or period has passed. CASA has determined that these A</span><span>Ds </span><span>may be applicable t</span><span>o</span><span> Australian aircraft. This Directive is issued</span><span> </span><span>to ensure all State of Design ADs are complied with.</span></p></td></tr><tr><td style="width:74.35pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span></span></p></td><td style="width:414.55pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p style="page-break-inside:avoid; page-break-after:avoid"><span>CASA appreciates that, due to date of aircraft manufacture or aircraft configuration and modification status, some of the ADs listed in Table 1 will not be applicable to some aeroplanes.</span><span>The original issue of this Directive applied only to A319 aeroplanes and became effective on 15 March 2007.</span></p><p><span>Amendment 1, extended the applicability to include A320 and A321 aeroplanes, amended the title of the AD, restricted applicability to aeroplanes manufactured prior to 1 January 2002, and incorporated an additional eight State of Design ADs.</span></p><p><span>Amendment 2 of this Directive removes obsolete website information and replaces </span><span>DGAC AD 1996-293(B)R1</span><span> with FAA AD 97-03-06 because the FAA is the </span><span>S</span><span>tate of </span><span>D</span><span>esign for the applicable equipment, and the FAA AD</span><span> address</span><span>es</span><span> the same unsafe condition</span><span>.</span></p></td></tr></tbody></table>