Boeing 717 Series AeroplanesBoeing 717 Series Aeroplanes

Boeing 717 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>Boeing Model 717-200 aeroplanes, fuselage numbers 5002 through 5134 inclusive.</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"><p style="margin-left:21.3pt; margin-bottom:12pt; text-indent:-21.3pt"><span>1.</span><span style="width:12.3pt; text-indent:0pt; display:inline-block"> </span><span>Replace the eight brake fuses of the hydraulic quantity limiter by doing either Option 1 or Option 2 in Table 1 of this Directive in accordance with Boeing Alert Service Bulletin 717-32A0031, dated 10 September 2004.</span></p><p style="margin-top:12pt; text-align:center"><span style="font-weight:bold">Table 1. - Replacement</span></p><table cellspacing="0" cellpadding="0" style="margin:0pt auto; border:0.75pt solid #000000; border-collapse:collapse"><tbody><tr style="height:39.7pt"><td style="width:63.5pt; border-right:0.75pt solid #000000; border-bottom:0.75pt solid #000000; vertical-align:middle"><p style="text-align:center"><span style="font-weight:bold">Option</span><br><span></span></p></td><td style="width:322pt; border-left:0.75pt solid #000000; border-bottom:0.75pt solid #000000; vertical-align:middle"><p style="text-align:center"><span style="font-weight:bold">Replace eight fuses having part number</span><br><span style="font-weight:bold">(P/N) 7918282-5503 with-</span></p></td></tr><tr style="height:28.4pt"><td style="width:63.5pt; border-top:0.75pt solid #000000; border-right:0.75pt solid #000000; border-bottom:0.75pt solid #000000; vertical-align:middle"><p style="text-align:center"><span>1</span></p></td><td style="width:322pt; border-top:0.75pt solid #000000; border-left:0.75pt solid #000000; border-bottom:0.75pt solid #000000; vertical-align:middle"><p style="margin-left:21.25pt"><span>New fuses having P/N 7918282-5505.</span></p></td></tr><tr style="height:26.3pt"><td style="width:63.5pt; border-top:0.75pt solid #000000; border-right:0.75pt solid #000000; vertical-align:middle"><p style="text-align:center"><span>2</span></p></td><td style="width:322pt; border-top:0.75pt solid #000000; border-left:0.75pt solid #000000; vertical-align:middle"><p style="margin-left:21.25pt"><span>Modified and reidentified fuses having P/N 7918282-5505.</span></p></td></tr></tbody></table><p class="Note" style="margin-bottom:12pt"><span>Note 1:</span><span> </span><span>Boeing Alert Service Bulletin 717-32A0031 refers to Parker Hannifin Corporation Stratoflex Products Division Service Bulletin 836SD-8-6-20, Revision 1, dated 23 June 2004, as an additional source of service information for modifying and reidentifying the brake fuses.</span></p><p style="margin-top:12pt; margin-left:21.3pt; margin-bottom:12pt; text-indent:-21.3pt"><span>2.</span><span style="width:12.3pt; text-indent:0pt; display:inline-block"> </span><span>Do not install a brake fuse, P/N 7918282-5503, on any aeroplane.</span></p><p class="Note" style="margin-top:12pt"><span>Note 2:</span><span> </span><span>FAA AD 2005-11-03 Amdt 39-14105 refers.</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 style="width:414.55pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><ol style="margin:0pt; padding-left:0pt"><li style="margin-left:14pt; margin-bottom:12pt; padding-left:7.25pt"><span>In accordance with Table 2 of this Directive.</span></li></ol><p style="margin-top:12pt; text-align:center"><span style="font-weight:bold">Table 2. - </span><span style="font-weight:bold">Compliance Times</span></p><table cellspacing="0" cellpadding="0" style="width:409pt; margin-top:0pt; margin-bottom:0pt; border:0.75pt solid #000000; border-collapse:collapse"><tbody><tr><td style="width:141pt; border-right:0.75pt solid #000000; border-bottom:0.75pt solid #000000; vertical-align:middle"><p style="text-align:center"><span>For aeroplanes having-</span></p></td><td style="width:141pt; border-left:0.75pt solid #000000; border-bottom:0.75pt solid #000000; vertical-align:middle"><p style="text-align:center"><span>Compliance time</span></p></td></tr><tr><td style="width:141pt; border-top:0.75pt solid #000000; border-right:0.75pt solid #000000; border-bottom:0.75pt solid #000000; vertical-align:middle"><p style="margin-left:6.7pt"><span>(1)</span><span> </span><span>Less than 5,000 total flight cycles as of the effective date of this Directive.</span></p></td><td style="width:141pt; border-top:0.75pt solid #000000; border-left:0.75pt solid #000000; border-bottom:0.75pt solid #000000; vertical-align:middle"><p style="margin-left:15.25pt"><span>Within 3,600 flight cycles after the effective date of this Directive.</span></p></td></tr><tr><td style="width:141pt; border-top:0.75pt solid #000000; border-right:0.75pt solid #000000; vertical-align:middle"><p style="margin-left:6.7pt"><span>(2)</span><span> </span><span>5,000 or more total flight cycles as of the effective date of this Directive.</span></p></td><td style="width:141pt; border-top:0.75pt solid #000000; border-left:0.75pt solid #000000; vertical-align:middle"><p style="margin-left:15.25pt"><span>Within 1,500 flight cycles after the effective date of this Directive.</span></p></td></tr></tbody></table><p style="margin-left:21.3pt; text-indent:-21.3pt"><span>2.</span><span style="width:12.3pt; text-indent:0pt; display:inline-block"> </span><span>After the effective date of this Directive.</span></p></td></tr></tbody></table>