04/01/2013 Page 1/462 - EASA

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EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10015329 LEARJET INC. EASA.IM.A.S.00322 FAA STC ST00151BO LEARJET 55 Installation of Honeywell CAS-67A TCAS II 1. FAA STC ST00151BO.2. This STC is 09.11.2004 Software Change 7,0. approved only for the product configuration as defined in the approved design data referred to in the paragraph "Description". Compatibility with other aircraft/engine configurations shall be determined by the ins 10015330 LEARJET INC. EASA.IM.A.S.00323 REV. 5 FAA STC SA8168NM-D CL-600-2B16 (CL-604) Installation of a Complete Custom Aircraft Interior 10015357 LEARJET INC. EASA.IM.A.S.0065 FAA STC ST01595LA-D BOMBARDIER BD-100-1A10 (CHALLE 10015359 LEARJET INC. EASA.IM.A.S.0066 FAA STC ST01603LA-D BOMBARDIER BD-100-1A10 (CHALLE 10015360 LEARJET INC. EASA.IM.A.S.0067 FAA STC ST01253LA-D BD-100-1A10 (CHALLENGER 300) 10015365 LEARJET INC. EASA.IM.A.S.0068 FAA STC ST01254LA-D BOMBARDIER BD-100-1A10 (CHALLE 10015392 LEARJET INC. EASA.IM.A.S.01091 FAA STC ST01619LA-D BOMBARDIER BD-100-1A10 (CHALLE 10015486 LEARJET INC. EASA.IM.A.S.01247 FAA STC ST01720LA-D LEARJET 31 LEARJET 35 LEARJET 35A LEARJET 36 LEARJET 36A Restricted to MSN 5449, 5510, 5523, 5539, 5572, 5577, 5585 The modification consists in the installation of 1. Modification of an aircraft by this Control Wheel Lighted Chart Holders, in supplemental Type Certificate obligates the accordance with Master Drawing List aircraft operator to include the maintenance HC33105000, Revision B, dated April 23, 2004 information provided by Document Number or later FAA approved revision.This STC is the HC33105000-IFCA-1 in the operator's Aircraft validation of the FAA approved STC No. Maintenance Manual and the operator's Ai The modification consists in the installation of a 1. Modification of an aircraft by this Service Panel Lighting System, in accordance Supplemental Type Certificate under -1 with Master Drawing List HC33315000, Configuration/installation, obligates the Revision A, dated june 03, 2004 or later FAA aircraftoperator to include the maintenance approved revision.This STC is the validation of information provided by Document Number the FAA approved STC No. ST016 HC33315000-IFCA-1 in the operator's Aircraft Main The modification consists in the installation of 1. Modification of an aircraft by this Cockpit Writing Tables, in accordance with Supplemental Type Certificate obligates the Master Drawing List HC31515000, Revision D, aircraft operator to include the maintenance dated December 18, 2003 or later FAA- information provided by Document Number approved revision.This STC is the validation of HC31515000-IFCA in the operator's Aircraft the FAA approved STC No. ST01253LA- Maintenance Manual and the operator's Airc The modification consists in the installation of 1. The Maintenance Instructions for an Artex ELT with Nav Interface in accordance Continued Airworthiness are contained in with Master Drawing List HC25615000,Rev. D Documents Number HC25615000-IFCA. dated December 19, 2003 (or later FAA Modification of an aircraft by this STC obligates approved revision).This STC is the validation of the aircraft operator to include the maintenance the FAA approved STC No. ST0125 information provided by this document in th Installation of an Executive Interior in accordance with Master Drawing List HC200335000 Revision D or later FAA approved revision Dual Honeywell MST-67A Diversity Transponders for Elementary & Enhanced Surveillance 10015532 LEARJET INC. EASA.IM.A.S.01412 FAA STC ST00190DE-D CL-600-2B16 Installation of Honeywell FMZ-2000 Flight Management System (FMS) with a Honeywell GNSSU 12 Channel GPS Sensor 1. The Maintenance Instructions for Continued Airworthiness are contained in Document Number HC200335000-IFCA-1. Modification of anaircraft by this STC obligates the aircraft operator to include the maintenance information provided by this document in the This STC is approved only for the product configuration as defined in the approved design data referred to in the paragraph "Description". Compatibility with other aircraft/engine configurations shall be determined by the installer. This STC is approved only for the product configuration as defined in the approved design data referred to in the paragraph "Description". Compatibility with other aircraft/engine configurations shall be determined by the 10015534 LEARJET INC. EASA.IM.A.S.01418 FAA STC ST01235LA-D BOMBARDIER CL-600-2B16 Universal Avionics TT-3000 AERO-M Satcom installer. This STC is approved only for the product System.Master Drawing List No. DC 23155002 configuration as defined in the approved design Revision E or later FAA approved revision data referred to in the paragraph "Description". Compatibility with other aircraft/engine configurations shall be determined by the installer. 10015535 LEARJET INC. EASA.IM.A.S.01419 FAA STC SA8195NM-D BOMBARDIER CL-600-2B16 Observer Audio Panel Installation.Master This STC is approved only for the product Drawing List No. DC23515000 Revision F or configuration as defined in the approved design later FAA approved revision. data referred to in the paragraph "Description". Compatibility with other aircraft/engine configurations shall be determined by the installer. Prior to installation of this modification it 04.03.2010 must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product. 04/01/2013 Page 306/462 28.07.2004 28.07.2004 28.07.2004 28.07.2004 24.01.2005 26.07.2005 26.07.2005 09.08.2005 09.08.2005
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10015536 LEARJET INC. EASA.IM.A.S.01420 FAA STC ST01258LA-D LEARJET 45 Installation of a Universal UMS-1C+ Flight 1. Universal UNS-1C FMS System must be 18.08.2005 Management System Upgrade from Software installed prior to installation of this STC.2. Control Number (SCN) 602.X to (SCN) 80X.X This STC is approved only for the product with Data Transfer Unit configuration as defined in the approved design data referred to in the paragraph "Description". Compatibility with other 10015537 LEARJET INC. EASA.IM.A.S.01421 FAA STC ST00412DE-D LEARJET 45 Installation of UNS-1C Flight Management System (Software Version 604.X) 10015549 LEARJET Inc. EASA.IM.A.S.01443 FAA STC ST01463SE LEARJET 31 Group Aircraft Approval for Reduced Vertical Separation Minimum (RVSM) 10015616 LEARJET INC. EASA.IM.A.S.01555 FAA STC SA8171NM-D BOMBARDIER BD-700-1A10 Pilot and Co-Pilot Footrests for BF700-1A10 Global Expressacc.: MDL GC2500501 Rev. B or later FAA approved rev.Validation of imported FAA STC: SA8171NM-D 10015710 LEARJET Inc. EASA.IM.A.S.01703 FAA STC ST01181WI-D LEARJET 31 LEARJET 35 LEARJET 35A LEARJET 36 LEARJET 36A Installation of Honeywell IHAS-800 Multi- Hazard Awareness System 10015730 LEARJET INC. EASA.IM.A.S.01749 FAA STC ST00342DE-D LEARJET 31A Installation of Single Universal Avionics Corporation UNS-1C FMS 10015788 LEARJET INC. EASA.IM.A.S.01844 FAA STC ST00508DE-D BOMBARDIER CL-600-2B16 Installation of Collins PCD-3000 Data Loader Interface System 10015790 LEARJET INC. EASA.IM.A.S.01848 FAA STC ST8139NM-D BOMBARDIER CL-600-2B16 Installation of a Collins VHF-22C Comm System with CTL-22C. 10015796 LEARJET INC. EASA.IM.A.S.01855 FAA STC ST01717LA-D BOMBARDIER BD-100-1A10 (CHALLE 10015817 LEARJET INC. EASA.IM.A.S.01888 REV. 1 SA06-10 BOMBARDIER BD-700-1A10 BOMBARDIER BD-700-1A11 10015852 LEARJET Inc. EASA.IM.A.S.01955 FAA STC ST01186WI-D LEARJET 31 LEARJET 35 LEARJET 35A LEARJET 36 LEARJET 36A 1. Instructions for Continued Airworthiness BAS-45010006-IFCA or BAS-45010006-IFC-2 dated March 28 2000 or later approved revision required for this installation.2. This STC is approved only for the product configuration as defined in the approved de This STC is approved only for the product configuration as defined in the approved design data referred to in the paragraph "Description". Compatibility with other aircraft/engine configurations shall be determined by the installer. Learjet Master Document List BAS35015037 Revision l or later approved revision - configurations -2, -4 and -5 only This STC is approved only for the product configuration as defined in the approved design data referred to in the paragraph "Description". Compatibility with other aircraft/engine configurations shall be determined by the installer. 1. This STC is approved only for the product configuration as defined in the approved design data referred to in the paragraph "Description". Compatibility with other aircraft/engine configurations shall be determined by the installer. This STC is approved only for the product configuration as defined in the approved design data referred to in the paragraphs "Description" and “Associated Technical Documentation”. Compatibility with other aircraft/engine configurations shall be determined installation of a lavatory Seat Modification - Belt Certification basis: a deviation from 25.789(b) replacement,in accordance with Master has been granted for personal injury criteria Drawing List BAS68010002, rev C testing of side singlw occupancy seats (Learjet CRI D-3) EGPWS Software Upgrade Installation of Cockpit Speaker Mute Installation of Universal UNS-1L Flight Management System. 1.The approval for the Master Document List - 1 configuration, EGPWS Software Upgrade (- 218-218 Software), is contingent on the aircraft being equipped with a previously EASA approved installation of a MK V Honeywell EGPWS with Version -206-206 Software or Not JAA TGL10 Compliant with present software load. 10015884 LEARJET INC. EASA.IM.A.S.02002 FAA STC SA8197NM-D BOMBARDIER CL-600-2B16 (604) Installation of Oxygen System-Passenger & crew (14500ft) -- 20.06.2006 10015919 LEARJET INC. EASA.IM.A.S.02052 ST01237LA-D BOMBARDIER CL-600-2B16 (CL- Installation of a Complete Custom Interior Modification of an aircraft by this STC obligates 03.11.2006 604 the aircraft operator to include the maintenance information TE-55325000-IFCA in the operators Maintenance Manual & the Operators Scheduled Maintenance ProgramThe equipment for which provisions were provide 04/01/2013 Page 307/462 18.08.2005 08.12.2005 16.11.2005 22.03.2006 02.01.2006 20.01.2006 07.05.2007 07.04.2006 03.06.2008 13.10.2006
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04/01/2013 Page 1/462 - EASA

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