Radio Communication and Navigation EquipRadio Communication and Navigation Equipment

Radio Communication and Navigation Equipment

<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="6" style="width:414.55pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>Honeywell RCZ-833J, RCZ-833K, RCZ-851J, RCZ-851K and RCZ-854J communications (COM) units and Honeywell XS-856A, XS-856B and XS-857A Mode S transponder units with the following part numbers (P/N):</span></p></td></tr><tr><td style="width:74.35pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p style="text-align:center"><span></span></p></td><td style="width:30.1pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p style="text-align:center"><span style="font-weight:bold"></span></p></td><td style="width:88.55pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p style="text-align:center"><span style="font-weight:bold">Communications Unit</span></p></td><td colspan="2" style="width:95.6pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p style="text-align:center"><span style="font-weight:bold">P/N</span></p></td><td style="width:74.35pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p style="text-align:center"><span style="font-weight:bold">Mode S Transponder</span></p></td><td style="width:83.15pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p style="text-align:center"><span style="font-weight:bold">P/N</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:30.1pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span></span></p></td><td style="width:88.55pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p style="text-align:center"><span>RCZ-833J</span><br><br><span>RCZ-833K</span><br><br><span>RCZ-851J</span><br><span>RCZ-851K</span><br><span>RCZ-854J</span></p></td><td colspan="2" style="width:95.6pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p style="text-align:center"><span>7510700-763</span><br><span>7510700-863</span><br><span>7510700-765</span><br><span>7510700-875</span><br><span>7510700-813</span><br><span>7510700-815</span><br><span>7510700-725</span><br><span>7510700-825</span></p></td><td style="width:74.35pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p style="text-align:center"><span>XS-856A</span><br><br><span>XS-856B</span><br><br><span>XS-857A</span></p></td><td style="width:83.15pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p style="text-align:center"><span>7517400-865</span><br><span>7517400-885</span><br><span>7517400-866</span><br><span>7517400-886</span><br><span>7517400-876</span><br><span>7517400-896</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="6" style="width:414.55pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p class="Note"><span>Note 1:</span><span> </span><span>These units are known to be fitted to, but not limited to, the following aeroplane models:</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:171.85pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p class="Note" style="text-align:center"><span style="font-weight:bold">Manufacturer</span></p></td><td colspan="3" style="width:232pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p class="Note" style="text-align:center"><span style="font-weight:bold">Model</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:171.85pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p class="Note" style="margin-left:42.55pt; text-indent:-42.55pt"><span style="width:42.55pt; text-indent:0pt; display:inline-block"></span><span>British Aerospace</span><br><span>Bombardier</span><br><span>Cessna</span><br><span>Dassault</span><br><span>Embraer</span><br><span>Learjet</span><br><span>Lockheed</span><br><span>Raytheon</span></p></td><td colspan="3" style="width:232pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p class="Note"><span>Jetstream 4100 series</span><br><span>BD-700-1A10 and BD-700-1A11</span><br><span>525, 550, 560 and 650 series</span><br><span>Falcon 900EX and 2000EX series</span><br><span>EMB-135 and EMB-145 series</span><br><span>45</span><br><span>282-44A-05 (C130B) and 382G series</span><br><span>Hawker 800 (including U-125A), 800XP and 1000 series</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="6" 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>For aircraft equipped with Honeywell RCZ-833J, RCZ-833K, RCZ-851J,</span><br><span>RCZ-851K or RCZ-854J COM units, with P/Ns listed in the applicability section 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="6" style="width:414.55pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p style="margin-left:42.55pt; text-indent:-21.3pt"><span>a.</span><span style="width:12.97pt; text-indent:0pt; display:inline-block"> </span><span>If not previously accomplished in accordance with AD/RAD/84 - Amend the applicable Aircraft Flight Manual (AFM) by inserting the following statement into the Normal Procedures Section:</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="6" style="width:414.55pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p style="margin-left:63.8pt"><span>“After completion of any 4096 ATC Code change (also referred to as Mode A Code), check the status of the transponder.</span><span> </span><span>If the transponder indicates that it is in standby mode, re-select the desired mode (i.e. the transponder should be in the active mode).”</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="6" style="width:414.55pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>Amendment of the AFM Normal Procedures Section may be accomplished by inserting a copy of this Directive 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="6" style="width:414.55pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p style="margin-left:42.55pt; text-indent:-21.3pt"><span>b.</span><span style="width:12.3pt; text-indent:0pt; display:inline-block"> </span><span>If not previously accomplished in accordance with AD/RAD/84 - Modify the COM unit by incorporating Honeywell Service Bulletin (SB) Publication No A21-3851-005 dated 29 July 2005 or Honeywell SB Publication No</span><br><span>A24-3851-002 dated 28 July 2005 as applicable.</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="6" style="width:414.55pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p class="Note"><span>Note 2:</span><span> </span><span>Accomplishment of the modification or replacement with a modified unit in accordance with the instructions contained in Honeywell Alert Service Bulletin (ASB) 7510700-23-A0048 dated 27 January 2006 and, as necessary, ASB</span><br><span>7517400-23-A6015 Revision 001 dated 29 July 2005 is an acceptable alternative to the Requirement1.b.modification.</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="6" style="width:414.55pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p style="margin-left:42.55pt; text-indent:-21.3pt"><span>c.</span><span style="width:12.97pt; text-indent:0pt; display:inline-block"> </span><span>Replace the XS-852E/F Mode S transponder of the COM unit with a new or modified XS-852E/F Mode S transponder that has MOD V installed, in accordance with Honeywell Alert Service Bulletin 7510700-23-A0047 Revision 001, dated July 29, 2005.</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="6" 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>For aircraft equipped with Honeywell XS-856A, XS-856B or XS-857A Mode S Transponder Units, with P/Ns listed in the applicability section 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="6" style="width:414.55pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p style="margin-left:42.55pt; text-indent:-21.25pt"><span>a.</span><span style="width:12.92pt; text-indent:0pt; display:inline-block"> </span><span>Unless already accomplished in accordance with Requirement 1.a. - Amend the applicable Aircraft Flight Manual (AFM) by inserting the following statement into the Normal Procedures Section:</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="6" style="width:414.55pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p style="margin-left:63.8pt"><span>“After completion of any 4096 ATC Code change (also referred to as Mode A Code), check the status of the transponder.</span><span> </span><span>If the transponder indicates that it is in standby mode, re-select the desired mode (i.e. the transponder should be in the active mode).”</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="6" style="width:414.55pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>Amendment of the AFM Normal Procedures Section may be accomplished by inserting a copy of this Directive 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="6" style="width:414.55pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p style="margin-left:42.55pt; text-indent:-21.3pt"><span>b.</span><span style="width:12.3pt; text-indent:0pt; display:inline-block"> </span><span>Unless already accomplished, replace the modification plate of the transponder with a new plate and test the transponder, in accordance with the Accomplishment Instructions of Honeywell ASB 7517400-23-A0017, dated 23</span><span> </span><span>January</span><span> </span><span>2006.</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="6" style="width:414.55pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p style="margin-left:42.55pt; text-indent:-21.3pt"><span>c.</span><span style="width:12.97pt; text-indent:0pt; display:inline-block"> </span><span>If the transponder fails the test specified in Requirement 2.b., install MOD Y into the transponder as specified in Requirement 2.d.</span></p></td></tr><tr style="height:0pt"><td style="width:85.05pt"></td><td style="width:40.8pt"></td><td style="width:99.25pt"></td><td style="width:42.5pt"></td><td style="width:63.8pt"></td><td style="width:85.05pt"></td><td style="width:93.85pt"></td></tr></tbody></table>