Division BAe Systems (Operations) Jetstream 4100 - AD/J4100/1 Amdt 1 - State of Design ADs - BAe Systems (Operations) Jetstream 4100 Series Aeroplanes | Zoe
<table cellspacing="0" cellpadding="0" style="width:510.68pt; margin-top:0pt; margin-bottom:0pt; border-collapse:collapse"><tbody><tr style="height:13.1pt"><td rowspan="14" style="width:74.35pt; border-right:0.75pt solid #000000; padding-right:4.97pt; padding-left:5.35pt; vertical-align:top"><p><span></span></p></td><td style="width:86.8pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p style="text-align:center"><span>006-09-98</span></p></td><td style="width:95.6pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p style="text-align:center"><span>11 September 1998</span></p></td><td style="width:210.75pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p><span>Elevator and Rudder Controls at Rear Pressure Bulkhead</span></p></td></tr><tr style="height:13.1pt"><td style="width:86.8pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p style="text-align:center"><span>005-04-99</span></p></td><td style="width:95.6pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p style="text-align:center"><span>5 April</span><span> </span><span>1999</span></p></td><td style="width:210.75pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p><span>Fuel - Distribution - Protection of the cable assembly to the fuel standby (boost) pump (left and right)</span></p></td></tr><tr style="height:13.1pt"><td style="width:86.8pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p style="text-align:center"><span>004-05-99</span></p></td><td style="width:95.6pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p style="text-align:center"><span>11 May 1999</span></p></td><td style="width:210.75pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p><span>Temporary Placard to Prohibit Aircraft Pushback with Engines Running</span></p></td></tr><tr style="height:13.1pt"><td style="width:86.8pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p style="text-align:center"><span>007-09-99</span></p></td><td style="width:95.6pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p style="text-align:center"><span>17 September 1999</span></p></td><td style="width:210.75pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p><span>Landing Gear - Inspection and rectification of main landing gear retract actuator ramrod piston retraining nut</span></p></td></tr><tr style="height:13.1pt"><td style="width:86.8pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p style="text-align:center"><span>002-03-2000</span></p></td><td style="width:95.6pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p style="text-align:center"><span>10 March 2000</span></p></td><td style="width:210.75pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p><span>Flight Controls - Rudder Pedals - Elimination of potential restricted movement of the rudder pedals</span></p></td></tr><tr style="height:13.1pt"><td style="width:86.8pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p style="text-align:center"><span>003-03-2000</span></p></td><td style="width:95.6pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p style="text-align:center"><span>15 March 200</span></p></td><td style="width:210.75pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p><span>Hydraulic Hand Pump Mounting Brackets</span></p></td></tr><tr style="height:13.1pt"><td style="width:86.8pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p style="text-align:center"><span>006-05-2000</span></p></td><td style="width:95.6pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p style="text-align:center"><span>31 May 2000</span></p></td><td style="width:210.75pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p><span>Flying Controls - Introduction of an elevator cable tension regulator incorporating secondary locking of the regulator</span></p></td></tr><tr style="height:13.1pt"><td style="width:86.8pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p style="text-align:center"><span>001-07-2001</span></p></td><td style="width:95.6pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p style="text-align:center"><span>3 July 2001</span></p></td><td style="width:210.75pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p><span>Nose Landing Gear Life limits</span></p></td></tr><tr style="height:13.1pt"><td style="width:86.8pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p style="text-align:center"><span>001-11-2001</span></p></td><td style="width:95.6pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p style="text-align:center"><span>5 November 2001</span></p></td><td style="width:210.75pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p><span>Propeller - Reduced performance due to loss of propeller efficiency</span></p></td></tr><tr style="height:13.1pt"><td style="width:86.8pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p style="text-align:center"><span>006-11-2001</span></p></td><td style="width:95.6pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p style="text-align:center"><span>7 November 2001</span></p></td><td style="width:210.75pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p><span>Flight Controls - Trim Screw Jack Chain Replacement</span></p></td></tr><tr style="height:13.1pt"><td style="width:86.8pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p style="text-align:center"><span>007-01-2002</span></p></td><td style="width:95.6pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p style="text-align:center"><span>24 January 2002</span></p></td><td style="width:210.75pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p><span>Main Landing Gear Door Drive</span><span> Trunnion Pins</span></p></td></tr><tr style="height:13.1pt"><td style="width:86.8pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p style="text-align:center"><span>006-08-2002</span></p></td><td style="width:95.6pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p style="text-align:center"><span>6 August 2002</span></p></td><td style="width:210.75pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p><span>Landing Gear - Introduction of overhaul lives for auxiliary components installed on the main and nose gear</span></p></td></tr><tr style="height:13.1pt"><td style="width:86.8pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p style="text-align:center"><span>006-06-2003</span></p></td><td style="width:95.6pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p style="text-align:center"><span>27 June 2003</span></p></td><td style="width:210.75pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p><span>Aileron Rear Spar</span></p></td></tr><tr style="height:13.1pt"><td style="width:86.8pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p style="text-align:center"><span>G-2005-0006</span></p></td><td style="width:95.6pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p style="text-align:center"><span>8 February 2005</span></p></td><td style="width:210.75pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p><span>ATA 24 - Electrical System - Modification</span></p></td></tr></tbody></table>
<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></span></p></td><td colspan="3" style="width:414.55pt; border-top:0.75pt solid #000000; border-bottom:0.75pt solid #000000; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p style="text-align:center"><span style="font-weight:bold">Table 2</span></p></td></tr><tr style="height:13.15pt"><td rowspan="2" style="width:74.35pt; border-right:0.75pt solid #000000; padding-right:4.97pt; padding-left:5.35pt; vertical-align:top"><p><span></span></p></td><td style="width:86.8pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p style="margin-left:21.3pt; text-indent:-21.3pt; text-align:center"><span style="font-weight:bold">EASA AD</span></p></td><td style="width:102.7pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p style="margin-left:21.3pt; text-indent:-21.3pt; text-align:center"><span style="font-weight:bold">Effective Date</span></p></td><td style="width:203.65pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p style="margin-left:21.3pt; text-indent:-21.3pt; text-align:center"><span style="font-weight:bold">Title</span></p></td></tr><tr style="height:13.1pt"><td style="width:86.8pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p style="margin-left:21.3pt; text-indent:-21.3pt"><span>2007-0268</span></p></td><td style="width:102.7pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p style="text-align:center"><span>22 October 2007</span></p></td><td style="width:203.65pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p><span>Placards & Marking - Propeller Limitations Placard - Replacement</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="3" style="width:414.55pt; border-top:0.75pt solid #000000; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p style="margin-bottom:12pt"><span style="font-style:italic">Note 1:</span><span style="font-style:italic"> </span><span style="font-style:italic">CAA(</span><span style="font-style:italic">UK</span><span style="font-style:italic">) and EASA ADs issued after28 September 2003 may be accessed via the internet at the following URL:</span></p><p class="Note" style="margin-top:12pt"><span style="width:36pt; display:inline-block"></span><span>http://ad.easa.europa.eu/</span><span></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="3" style="width:414.55pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p style="margin-bottom:12pt"><span style="font-style:italic">Note 2:</span><span style="font-style:italic"> </span><span style="font-style:italic">CAA(</span><span style="font-style:italic">UK</span><span style="font-style:italic">) ADs issued before 28 September 2003</span><span style="font-weight:bold; font-style:italic"> </span><span style="font-style:italic">are listed in CAA(</span><span style="font-style:italic">UK</span><span style="font-style:italic">)</span><br><span style="font-style:italic">CAP 476 which may be accessed via the internet, by following the links at the following URL:</span></p><p style="margin-top:12pt"><span style="width:36pt; display:inline-block"></span><span style="font-style:italic">http://www.caa.co.uk/default.aspx?catid=1443&pagetype=90</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="3" style="width:414.55pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span style="font-style:italic">Note 3:</span><span style="font-style:italic"> </span><span style="font-style:italic">Australian ADs previously issued in the CAO 105 AD/J41 series are no longer effective.</span><span style="font-style:italic"> </span><span style="font-style:italic">However these ADs will be reviewed and, if necessary, will be reissued in this series.</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 Requirements 1 and 2 - Within 30 days after the effective date of this Directive or prior to the issue of a Certificate of Airworthiness, 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="3" style="width:414.55pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>This Amendment becomes effective on 20 February 2008.</span></p></td></tr><tr><td style="width:74.35pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>Background:</span></p></td><td colspan="3" style="width:414.55pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>The ADs listed in Table 1 and 2 of this Directive require either one time actions for which the compliance date and/or period has passed or multiple inspection/actions until a terminating action has been applied and the compliance date and/or period for the terminating action has passed.</span><span> </span><span>CASA has determined that these ADs may be applicable to recently registered or imported Australian aircraft.</span><span> </span><span>This Directive is issued to ensure all previous State of </span><span>Design ADs</span><span> are complied with.</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>CASA appreciates that, due to date of aircraft manufacture or aircraft configuration and modification status, not all the ADs listed in Table 1 and 2 will be applicable to all Jetstream 4100 model aeroplanes.</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>The original issue of the Directive only listed two ADs, advice from EASA has indicated that additional applicable CAA(UK) ADs were listed in CAP 476.</span><span> </span><span>This Amendment lis</span><span>ts additional ADs from CAP 476.</span></p></td></tr></tbody></table>
The original issue of this Directive became effective on 31 January 2008.
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David Punshon
Delegate of the Civil Aviation Safety Authority