Univair Aircraft (Stinson) 108 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 colspan="2" style="width:414.55pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>All </span><span>Univair</span><span> Aircraft Corporation </span><span>Stinson Model 108 series aircraft.</span></p></td></tr><tr><td rowspan="7" style="width:74.35pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>Requirement:</span></p></td><td colspan="2" style="width:414.55pt; border-bottom:0.75pt solid #000000; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p style="margin-left:21.6pt; text-indent:-21.6pt"><span>1.</span><span style="width:12.6pt; text-indent:0pt; display:inline-block"> </span><span>Determine from Aircraft Records if the </span><span>requirements of the </span><span>F</span><span>ederal Aviation Administration of the United States of America (F</span><span>AA</span><span>)</span><span> Airworthiness Directives</span><span>, as in force at the time of issue of this AD,</span><span> </span><span>specified </span><span>in </span><span>T</span><span>able </span><span>1 of this AD </span><span>have been </span><span>carried out</span><span>.</span></p><p style="margin-left:21.6pt; text-indent:-21.6pt"><span>2.</span><span style="width:12.6pt; text-indent:0pt; display:inline-block"> </span><span>If it is determined that an FAA AD listed in Table 1 and as in force at the time of issue of this AD, is applicable and has not been previously complied with, then perform the actions required by that AD.</span></p></td></tr><tr style="height:5.1pt"><td style="width:143.5pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p style="margin-left:21.6pt; text-indent:-21.6pt; text-align:center"><span>Airworthiness Directive</span></p></td><td style="width:260.35pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p style="margin-left:21.6pt; text-indent:-21.6pt; text-align:center"><span>Subject</span></p></td></tr><tr style="height:5.1pt"><td style="width:143.5pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p style="margin-left:21.6pt; text-indent:-21.6pt; text-align:center"><span>FAA AD 47-50-11</span></p></td><td style="width:260.35pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p style="margin-left:21.6pt; text-indent:-21.6pt"><span>Front Ash Tray Modification or Placard Installation</span></p></td></tr><tr style="height:5.1pt"><td style="width:143.5pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p style="margin-left:21.6pt; text-indent:-21.6pt; text-align:center"><span>FAA AD 49-16-02</span></p></td><td style="width:260.35pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p style="margin-left:21.6pt; text-indent:-21.6pt"><span>Wing Fabric - Inspection and Rectification</span></p></td></tr><tr style="height:5.1pt"><td style="width:143.5pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p style="margin-left:21.6pt; text-indent:-21.6pt; text-align:center"><span>FAA AD 50-25-01</span></p></td><td style="width:260.35pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p style="margin-left:21.6pt; text-indent:-21.6pt"><span>Fuel Drip Strip Installation</span></p></td></tr><tr style="height:5.1pt"><td style="width:143.5pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p style="margin-left:21.6pt; text-indent:-21.6pt; text-align:center"><span>FAA AD 54-02-02</span></p></td><td style="width:260.35pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p style="margin-left:21.6pt; text-indent:-21.6pt"><span>Wheel Skis - Rigging</span><span>.</span></p></td></tr><tr style="height:5.1pt"><td colspan="2" style="width:414.55pt; border-top:0.75pt solid #000000; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p style="margin-left:21.6pt; text-indent:-21.6pt; text-align:center"><span>Table 1 - FAA Airworthiness Directives</span></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 colspan="2" style="width:414.55pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>If a certificate of airworthiness (</span><span>CofA</span><span>) has not been issued for the aircraft - accomplish before the issue of the </span><span>CofA</span><span>.</span></p><p><span>If a </span><span>CofA</span><span> has been issued for the aircraft - within </span><span>6</span><span>0 days after the </span><span>commencement</span><span> date of this Directive.</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 colspan="2" style="width:414.55pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>Th</span><span>is</span><span> </span><span>AD commences</span><span> </span><span>on</span><span> 31 August 2018</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 colspan="2" style="width:414.55pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>A review of the </span><span>Australian </span><span>Aircraft Register found that this aircraft type has been </span><span>registered </span><span>in Australia since 1987. There are currently 12 aircraft of this type on the register with the majority having been registered in 1994/95.</span></p><p><span>This AD is issued to ensure that compliance with these AD’s has been accomplished for aircraft imported into Australia.</span></p><p><span>The FAA ADs listed in Table 1 of this Directive require once-only actions for which the compliance date and/or period has passed. CASA has determined that these ADs may be applicable to recently registered Stinson model 108 aircraft.</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 colspan="2" style="width:414.55pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>CASA acknowledges 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 aircraft.</span></p></td></tr></tbody></table>