Bombardier (Canadair) CL-600 (ChallengerBombardier (Canadair) CL-600 (Challenger) Series Aeroplanes

Bombardier (Canadair) CL-600 (Challenger) Series Aeroplanes

<table cellspacing="0" cellpadding="0" style="width:510.35pt; margin-top:0pt; margin-bottom:0pt; border-collapse:collapse"><tbody><tr><td colspan="2" style="width:93.85pt; padding-right:5.4pt; padding-left:5.4pt; vertical-align:top"><h2 id="navPoint_2"><span>AD/CL-600/36 </span><span>Amdt</span><span> 1</span></h2></td><td style="width:315.2pt; padding-right:5.4pt; padding-left:5.4pt; vertical-align:top"><h2 id="navPoint_3" style="text-align:center"><span>Elevator Flutter Damper Shear Pins</span></h2></td><td style="width:68.3pt; padding-right:5.4pt; padding-left:5.4pt; vertical-align:top"><h2 id="navPoint_4"><span>14/2013</span></h2></td><td style="vertical-align:top"></td></tr><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:414.6pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>Model CL-600-2B19 “Regional Jet” aircraft, serial numbers 7003 through 7357.</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:414.6pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p style="margin-left:14.2pt; text-indent:-14.2pt"><span>1.</span><span style="width:5.2pt; text-indent:0pt; display:inline-block"> </span><span>For aircraft serial number 7003 through 7142, and 7144:</span></p><p style="margin-left:14.2pt"><span>Install new shear pins part number 601R24063-31/S in accordance with paragraph 2, Accomplishment Instructions, Part A of Bombardier Service Bulletin (SB) 601R-27-100, dated 22 December 1999.</span></p><p style="margin-left:14.2pt"><span>Upon accomplishment of the above requirement, the additional first flight of the day checks of the elevator control system as described in TR RJ/68-1, dated 15 February 2000, are no longer required and TR RJ/68-1 can be removed from the Aircraft Flight Manual.</span></p><p style="margin-left:14.2pt; text-indent:-14.2pt"><span>2.</span><span style="width:5.2pt; text-indent:0pt; display:inline-block"> </span><span>For aircraft serial number 7143, and 7145 through 7357:</span></p><p style="margin-left:14.2pt"><span>Review the aircraft maintenance logbook or records in accordance with paragraph 2, Accomplishment Instructions, Part B of Bombardier SB 601R-27-100, to determine if any elevator flutter damper shear pins have been replaced since aircraft delivery.</span></p><p style="margin-left:14.2pt"><span>If no elevator flutter damper shear pins have been replaced or if the shear pins have been replaced with part number 601R24063-31/S, no further action is required.</span></p><p style="margin-left:14.2pt; text-indent:-14.2pt"><span>3.</span><span style="width:5.2pt; text-indent:0pt; display:inline-block"> </span><span>If it cannot be verified that new elevator flutter damper shear pins part number 601R24063-31/S were installed, accomplish the following:</span></p><p style="margin-left:28.35pt; text-indent:-14.2pt"><span>a.</span><span style="width:5.87pt; text-indent:0pt; display:inline-block"> </span><span>Insert a copy of TR RJ/68-1 into the Aircraft Flight Manual and advise the flight crew of additional first flight of the day checks of the elevator control system as described in TR RJ/68-1.</span></p><p style="margin-left:28.4pt; text-indent:-14.2pt"><span>b.</span><span style="width:5.2pt; text-indent:0pt; display:inline-block"> </span><span>Install new shear pins part number 601R24063-31/S in accordance with paragraph 2, Accomplishment Instructions, Part C of SB 601R-27-100.</span></p></td></tr><tr style="height:0pt"><td style="width:85.05pt"></td><td style="width:19.6pt"></td><td style="width:326pt"></td><td style="width:79.1pt"></td><td style="width:0.6pt"></td></tr></tbody></table>