Cessna 550 (Citation II) Series AeroplanCessna 550 (Citation II) Series Aeroplanes

Cessna 550 (Citation II) 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>Model 550, 551 and S550 aeroplanes as identified in the following Cessna Service Bulletins (SB):</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:95.6pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p style="margin-left:36pt; margin-bottom:12pt; text-indent:-36pt; text-align:center"><span style="font-weight:bold">Model</span></p><p style="margin-top:12pt; text-align:center"><span>550</span><br><span>551</span><br><span>S550</span></p></td><td style="width:95.6pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p style="margin-left:36pt; margin-bottom:12pt; text-indent:-36pt; text-align:center"><span style="font-weight:bold">SB</span></p><p style="margin-top:12pt; text-align:center"><span>SB550-26-05</span><br><span>SB550-26-05</span><br><span>SBS550-26-02</span></p></td><td style="width:95.6pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p style="margin-left:36pt; margin-bottom:12pt; text-indent:-36pt; text-align:center"><span style="font-weight:bold">Revision</span></p><p style="margin-top:12pt; text-align:center"><span>Original</span><br><span>Original</span><br><span>Original</span></p></td><td style="width:95.65pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p style="margin-left:36pt; margin-bottom:12pt; text-indent:-36pt; text-align:center"><span style="font-weight:bold">Date</span></p><p style="margin-top:12pt; text-align:center"><span>1 April 2005</span><br><span>1 April 2005</span><br><span>1 April 2005</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 class="Note" style="margin-left:21.3pt; text-indent:-21.3pt"><span style="font-style:normal">1.</span><span style="width:12.3pt; text-indent:0pt; display:inline-block"> </span><span style="font-style:normal">If not previously accomplished in accordance with the original issue of this Directive, install identification sleeves on the wires for the positive and negative terminal studs of the engine fire extinguishing bottles; re-connect the wires to the correct studs; test the connection and re-connect the wires again as applicable until the connection tests correctly.</span><span style="font-style:normal"> </span><span style="font-style:normal">The above actions are to be accomplished in accordance with Cessna SB550-26-05 or SBS550-26-02 as applicable.</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" style="margin-left:21.3pt; text-indent:-21.3pt"><span style="font-style:normal">2.</span><span style="width:12.3pt; text-indent:0pt; display:inline-block"> </span><span style="font-style:normal">Fire extinguisher bottles may not be installed, as replacement spares, on any Cessna Model 550, 551 or S550 aeroplane unless identification sleeves have been installed on the wires for the positive and negative terminal studs in accordance with Requirement 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><span>Later revisions of the above SB(s), approved by the United States Federal Aviation Administration (FAA) as an Alternate Method of Compliance (AMOC) to FAA AD 2007-11-17, are considered acceptable for compliance with the equivalent Requirements 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 class="Note"><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>FAA AD 2007-11-17 Amdt 39-15074 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>For Requirement 1 - Within 100 hours time in service or 60 days after the effective date of this Amendment, whichever occurs first.</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>For Requirement 2 - As of the effective date of this Amendment.</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 Amendment becomes effective on 2 August 2007.</span></p></td></tr></tbody></table>