Gates Learjet 35 and 36 Series AeroplaneGates Learjet 35 and 36 Series Aeroplanes

Gates Learjet 35 and 36 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="3" style="width:414.55pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>Learjet model 35, 35A, 36 and 36A aeroplanes identified in Bombardier Service Bulletin (SB) 35/36-28-11 Revision 4 dated 4 December 2000.</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="3" style="width:414.55pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p style="margin-left:21.3pt; text-indent:-21.3pt"><span>1.</span><span style="width:12.3pt; text-indent:0pt; display:inline-block"> </span><span>Modify the left- and right-hand standby fuel pump switches, in accordance with the Accomplishment Instructions of SB 35/36-28-11 Revision 4.</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="3" style="width:414.55pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>Later revisions of the above SB, approved by the United States Federal Aviation Administration (FAA) as an Alternate Method of Compliance (AMOC) to FAA AD 2007-04-18, is/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><span></span></p></td><td colspan="3" style="width:414.55pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><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>Revise the Emergency and Abnormal Procedures sections of the applicable Learjet Aircraft Flight Manual (AFM) to advise the flight crew of proper procedures to follow in the event of failure of the standby fuel pump to shut off by including the information in the applicable Learjet Temporary Flight Manual (TFM) changes identified below:</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:131.05pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p style="margin-bottom:12pt"><span style="width:36pt; display:inline-block"></span><span style="font-weight:bold">TFM Change</span></p><p style="margin-top:12pt; margin-left:36pt; margin-bottom:12pt; text-indent:-36pt"><span style="width:36pt; text-indent:0pt; display:inline-block"></span><span>TFM 96-08</span><br><br><span></span></p><p style="margin-top:12pt; margin-left:36pt; text-indent:-0.55pt"><span>TFM 96-09</span></p></td><td style="width:79.7pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p style="margin-bottom:12pt; text-align:center"><span style="font-weight:bold">Date</span></p><p style="margin-top:12pt; margin-bottom:12pt"><span>30 May 1996</span><br><br><span></span></p><p style="margin-top:12pt"><span>30 May 1996</span></p></td><td style="width:182.4pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p style="margin-left:36pt; margin-bottom:12pt; text-indent:-36pt"><span style="width:36pt; text-indent:0pt; display:inline-block"></span><span style="font-weight:bold">AFM</span></p><p style="margin-top:12pt; margin-bottom:12pt"><span>35/36 (FM-019)</span><br><span>35A/36A FC-</span><span>200 (FM-102)</span><br><span>35A/36A FC-530 (FM-108)</span></p><p style="margin-top:12pt"><span>35/36 (FM-019)</span><br><span>35A/36A FC-200 (FM-102)</span><br><span>35A/36A FC-530 (FM-108)</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="3" style="width:414.55pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>This may be accomplished by inserting a copy of the TFM changes into the AFM.</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="3" style="width:414.55pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>When the TFM changes have been included in the general revisions of the AFM, those general revisions may be inserted into the AFM, provided the relevant information in the general revisions is identical to that in the TFM changes.</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="3" 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 2007-04-18 Amdt 39-14950 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="3" style="width:414.55pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>For Requirement 1 - Within 24 months after the effective date of this Directive.</span></p></td></tr></tbody></table>