General Electric Turbine Engines - CJ610 Series

<table cellspacing="0" cellpadding="0" style="width:510.3pt; margin-top:0pt; margin-bottom:0pt; border-collapse:collapse"><tbody><tr><td style="width:72.65pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>Applicability:</span></p></td><td colspan="2" style="width:416.25pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>General Electric Company (GE) CJ610 series turbojet engines.</span></p></td></tr><tr><td style="width:72.65pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>Requirement:</span></p></td><td colspan="2" style="width:416.25pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p class="Note" style="margin-left:21.6pt; text-indent:-21.6pt"><span style="font-style:normal">1.</span><span style="width:12.6pt; text-indent:0pt; display:inline-block"> </span><span style="font-style:normal">Determine the applicability of the United States of America Federal Aviation Administration </span><span style="font-weight:bold; font-style:normal">(</span><span style="font-weight:bold">FAA</span><span style="font-weight:bold; font-style:normal">)</span><span style="font-style:normal"> Airworthiness Directives (ADs) listed in Table 1, as in force from time to time.</span></p><p class="Note" style="margin-left:21.6pt; text-indent:-21.6pt"><span style="font-style:normal">2.</span><span style="width:12.6pt; text-indent:0pt; display:inline-block"> </span><span style="font-style:normal">If it is determined that an FAA AD listed in Table 1 is applicable and has not been previously accomplished, perform the actions required by that AD.</span></p><p class="Note" style="margin-left:1.8pt"><span>Note 1:</span><span> </span><span>The words “as in force from time to time” require compliance with the most recent version of the referenced document.</span></p></td></tr><tr><td style="width:72.65pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span></span></p></td><td colspan="2" style="width:416.25pt; border-bottom:0.75pt solid #000000; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p style="text-align:center"><span style="font-weight:bold">Table 1</span></p></td></tr><tr style="height:6.45pt"><td rowspan="7" style="width:72.65pt; border-right:0.75pt solid #000000; padding-right:4.97pt; padding-left:5.35pt; vertical-align:top"><p><span></span></p></td><td style="width:81.4pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p style="text-align:center"><span style="font-weight:bold">FAA AD</span></p></td><td style="width:324.15pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p style="text-align:center"><span style="font-weight:bold">Title</span></p></td></tr><tr style="height:6.35pt"><td style="width:81.4pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p style="text-align:center"><span>75-19-05</span></p></td><td style="width:324.15pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p><span>Accessory Drive Horizontal Drive Shaft – Inspection / Replacement</span></p></td></tr><tr style="height:6.35pt"><td style="width:81.4pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p style="text-align:center"><span>80-08-06R1</span></p></td><td style="width:324.15pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p><span>First Stage Turbine Disks and Second Stage Turbine Disks - Replacement</span></p></td></tr><tr style="height:6.35pt"><td style="width:81.4pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p style="text-align:center"><span>85-18-03</span></p></td><td style="width:324.15pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p><span>Stage 1 Turbine Disk - Replacement</span></p></td></tr><tr style="height:6.35pt"><td style="width:81.4pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p style="text-align:center"><span>97-25-08</span></p></td><td style="width:324.15pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p><span>Turbine Torque Ring and Compressor Drive Shaft - Replacement</span></p></td></tr><tr style="height:6.35pt"><td style="width:81.4pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p style="text-align:center"><span>98-23-06</span></p></td><td style="width:324.15pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p><span>Combustor Liner Assembly - Replacement</span></p></td></tr><tr style="height:6.35pt"><td style="width:81.4pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p style="text-align:center"><span>2001-10-12</span></p></td><td style="width:324.15pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p><span>Unapproved Parts - Removal from Service</span></p></td></tr><tr><td style="width:72.65pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>Compliance:</span></p></td><td colspan="2" style="width:416.25pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>For Requirements 1 and 2 - Within 30 days after the commencement date of this Directive.</span></p></td></tr><tr><td style="width:72.65pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span></span></p></td><td colspan="2" style="width:416.25pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>This AD commences on 15 July 2022.</span></p></td></tr><tr><td style="width:72.65pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>Background:</span></p></td><td colspan="2" style="width:416.25pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>The FAA ADs listed in Table 1 of this Directive require one-time actions for which the compliance date and/or period has passed. CASA has determined that these ADs may be applicable to recently registered Australian aircraft. This Directive is issued to ensure all State of Design ADs are complied with.</span></p></td></tr></tbody></table>

Delegate Signature

David Punshon
Delegate of the Civil Aviation Safety Authority

5 July 2022