Embraer EMB-135 and EMB-145 Series AeropEmbraer EMB-135 and EMB-145 Series Aeroplanes

Embraer EMB-135 and EMB-145 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="4" style="width:414.55pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>EMB-145XR model aircraft with serial numbers listed in Table 1.</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="4" style="width:414.55pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p style="margin-left:163.05pt"><span style="font-weight:bold">Table 1</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:101pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>145590</span><br><span>145643</span><br><span>145645</span><br><span>145646</span><br><span>145649</span><br><span>145650</span><br><span>145654</span><br><span>145655</span><br><span>145657 thru 145660</span><br><span>145662</span><br><span>145664</span><br><span>145666</span><br><span>145672</span><br><span>145674</span><br><span>145675</span></p></td><td style="width:102.7pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>145677</span><br><span>145681</span><br><span>145683</span><br><span>145684</span><br><span>145688 thru 145690</span><br><span>145693</span><br><span>145697</span><br><span>145700</span><br><span>145703 thru 145705</span><br><span>145708</span><br><span>145712</span><br><span>145714</span><br><span>145718</span><br><span>145719</span><br><span>145721</span></p></td><td style="width:102.7pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>145727</span><br><span>145731 thru 145733</span><br><span>145735</span><br><span>145739</span><br><span>145741</span><br><span>145745</span><br><span>145746</span><br><span>145749</span><br><span>145751</span><br><span>145753</span><br><span>145756</span><br><span>145758</span><br><span>145759</span><br><span>145761</span><br><span>145772</span></p></td><td style="width:76.05pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>145782</span><br><span>145786</span><br><span>145787</span><br><span>145791</span><br><span>145792</span><br><span>145799</span><br><span>14500805</span><br><span>14500808</span><br><span>14500811</span><br><span>14500817</span><br><span>14500819</span><br><span>14500831</span><br><span>14500834</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 colspan="4" style="width:414.55pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>Unless previously accomplished, install a bonding jumper between the pilot valve line tube and the pressure refuelling system tube, after removing ventral fuel tank access panel 196FR, as described in the Embraer Service Bulletin 145-28-0026, original issue, or further revisions approved by the Brazilian </span><span>Agência Nacional de Aviação Civil (</span><span>ANAC).</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="4" style="width:414.55pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p class="Note"><span>Note:</span><span> </span><span>ANAC AD 2006-12-01 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 colspan="4" style="width:414.55pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>Within the next 10,000 hours time in service (TIS) for aircraft with less than 5,000 hours TIS, or within the next 5,000 hours TIS for aircraft with more than 5,000 hours, TIS after 4 January 2007 (the effective date ANAC AD 2006-12-01).</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="4" style="width:414.55pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>This Airworthiness Directive becomes effective on 31 July 2008.</span></p></td></tr></tbody></table>