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 10016672 AVIDYNE CORPORATION EASA.IM.A.S.03174 FAA STC SA02013CH CIRRUS SR20 Installation of Avidyne Model 9900BX/ TAS 1) Prior to installation of this modification the 27.05.2009 CIRRUS SR22 600 Series Traffic Advisory System (TAS) installer must determine that the interrelationship between this modification andany other previously installed modification will introduce no adverse effect upon the airworthiness of the product.2) The ins 10030294 AVIDYNE CORPORATION REV. 1 FAA STC SA00269BO 1. SR20, SR22 2.SR22T Installation of Avidyne 700-00033-() Tactical Weather Detection System 10033140 AVIDYNE CORPORATION FAA STC SA00296BO SR20, SR22 Installation of Avidyne Model DFC90 Autopilot P/N 700-00170-000 System As indicated in FAA STC SA00269BO AML limited to Cirrus Design Corporation SR20, SR22, SR22T only. Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introdu as indicated in FAA STC SA00296BOAvidyne software P/N 530-00214-() Rev 02 or later FAA approved revisionwith underspeed protection functionality must be installed on PFD P/N700-00006-() 10038669 AVIDYNE CORPORATION FAA STC SA00310BO PA46-350P, PA-46R-350T Autopilot Series / DFC 90 Autopilot P/N 700- Aircraft must be configured with an existing S- 00170-002 DFC100 AutopilotP/N 700-00170- TEC 55X (or 55SR)Autopilot and with an 003 as replacement for the S-Tec System 55X existing Avidyne Flight Display System as Autopilot P/N1192-()-() in accordance with followsin order to accomplish this STC:For Avidyne Corporation Master Document DFC90: Avidyne Primary Flight Display, p/n ListAVDFC-077 700-00006-( ), loadedwith Release 8.0.4 so 10039607 AVIDYNE CORPORATION REV. 1 FAA STC SA0282BO PA-46R-350T Integrated Flight Display Enhanced Vision System (EVS) is not included in the scope of thisapprovalCompatibility with Mode 5 alerts must be shown when a TAWS Class A isinstalled. 10041185 AVIDYNE CORPORATION FAA STC SA00282BO SR20, SR22 Installation of Avidyne Corporation 700-00083- XXX Entegra IntegratedFlight Display System on Cirrus SR20 and SR22 according Avidyne Doc. NoAVIFD-006 in latest FAA approved Revision As indicated in FAA STC SA00282BOEnhanced Vision System (EVS) is not included in the scope of thisapprovalCompatibility with Mode 5 alerts must be shown when a TAWS Class A isinstalled. 21.12.2010 Prior to installation of this modification it 20.12.2010 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 productIf the h The approval holder shall fulfill the obligations of Part 21,Paragraph 21.A109.Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or 06.03.2012 Prior to installation of this modification it 11.10.2012 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. Prior to installation of this modification it 28.08.2012 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. If the 10042507 AVIDYNE CORPORATION FAA STC SA00323BO 182E, 182F, 182G, 182H, 182J, Installation of Avidyne Corporation Autopilot; Operation must be in accordance with Avidyne The installation of this modification by 05.12.2012 182K, 182L, 182M, 182N, 182P, model DFC90, p/n700-00170-022 (28-Volt Corporation AFMS documentNo. 600-00293- third persons is subject towritten 182R, 182S, 182T, R182. Electrical system) or p/n 700-00170-024 (14- 000, rev.00 dated 01-October-2012.The AFMS permission of the approval holder and VoltElectrical system), loaded with Release 0 must be carried in the Aircraft during all disposal of the approvedappropriate Software, as a replacement forthe S-Tec flights.Maintenance must be in accordance with documentation.Prior to installation of this Autopilot. ICA document AVDFC-125, rev.00dated 09- modification it must be determined thatthe interrelationship b 10042851 AVION RESEARCH, Inc. REV. 1 FAA STC SA170CH 1. 172 Installation of a Control Yoke and Instrument None 1. A copy of this certificate or later FAA 21.12.2012 1. 172A/B/C/D/E/F/G/H/I/K/L/M Panel in accordance withFAA STC SA170CH approved revision must bemaintained as 2. 175, 175A/B/C part of the permanent records for the modified aircraft.2. If the holder agrees to permit another person to use this certificateto alter the product, the holder shall give th 10014692 AVIONES, PIEZAS Y ACCESORIOS, S.L. EASA.A.S.02857 PIPER PA-31 Installation Dual integrated NAV/COMM/GPS GARMIN 480 and Transponder GARMIN GTX 33 (APA OT 5001 Rev.1). 05.02.2008 10014704 AVIONES, PIEZAS Y ACCESORIOS, S.L. EASA.A.S.02875 MITSUBISHI MU-2B-35 Installation of New Avionics Equipment to comply with COM/NAV regulations for IFR and B-RNAV Operation. 04/01/2013 Page 96/462 10.12.2007
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10017246 AVIONES, PIEZAS Y ACCESORIOS, S.L. EASA.R.S.01443 EUROCOPTER FRANCE AS 355 HD I. Ponti Radio Digital video, audio & data Prior to installation of this modification the 08.09.2008 SERIE Transmission System. installer must determine that the interrelationship between this modification and any other previously installed modification will introduce no adverse effect upon the airworthiness of the product. The install 10015426 AVIONICS GROUP INC. EASA.IM.A.S.01159 REV. 1 FAA STC ST02198AT B757-200, -200CB, -200PF Installation of a Teledyne Digital Flight Data Acquisition Unit, PartNumber 2233000-811 10016034 AVIONICS GROUP INC. EASA.IM.A.S.02203 ST02997AT BOEING 737-100 BOEING 737-200 BOEING 737-300 BOEING 737-400 BOEING 737-500 Installation of a Sandal Avionics ST3400 Class A Terrain Awareness and Warning System 10038339 AVIONICS GROUP INC. FAA STC ST03559AT 767-200, -300, -300F, -400ER Installation of Honeywell (TRA-67A) or Collins (TPR901) Mode S EnhancedSurveillance System 10014572 AVIONICS INTEGRATION & ENGINEERING 10014701 AVIONICS INTEGRATION & ENGINEERING 10014739 AVIONICS INTEGRATION & ENGINEERING 10014793 AVIONICS INTEGRATION & ENGINEERING 10014815 AVIONICS INTEGRATION & ENGINEERING 10014912 AVIONICS INTEGRATION & ENGINEERING 10014913 AVIONICS INTEGRATION & ENGINEERING 10014917 AVIONICS INTEGRATION & ENGINEERING 10014925 AVIONICS INTEGRATION & ENGINEERING 10014932 AVIONICS INTEGRATION & ENGINEERING 10014959 AVIONICS INTEGRATION & ENGINEERING 10015026 AVIONICS INTEGRATION & ENGINEERING None Prior to installation of this modification it 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 08.02.2011 FAA approved Airplane Flight Manual Supplement for Avionics Group, Inc. Sandel Avionics ST3400 Class A Terrain Awareness and Warning System dated December 8, 2004 is a required part of this STC. 31.10.2006 None Prior to installation of this modification it 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 08.02.2012 EASA.A.S.02676 BAE 125 -800 Replacement of Dual FMS UNS-1D by Dual -- 21.09.2006 HAWKER 800 SERIES UNS-1F, to allow the aircraft to comply with PR- NAV requirements. EASA.A.S.02870 BEECH B200 SUPER KING AIR Installation of a UASC Flight Management System (FMS) UNS-1L 24.01.2007 EASA.A.S.02922 BEECH B300 Standby Instruments InstallationIn: 2" Revue Thommen Standby Altimeter & 2" Revue Thommen Airspeed Indicator & L3 Communications Standby Attitude Indicator AI- 804with Goodrich JET Emergency Power Supply Battery Pack PS-835 11.05.2007 EASA.A.S.02995 REV 1 BEECH 400A Upgrade of existing FID capable dual TDR-94D 1. This change is limited to the configuration 04.04.2007 Mode S transponder system to enhanced of aircraft / equipment type as listed under Item surveillance capability by incorporation of 1.2 in Engineering Order, Doc. No. CV649- Collins SB 502 and SB 507. 062, Revision A, dated 23 March 2007, or later approved issue.2. This STC is approved only for the product confi EASA.A.S.03023 BOMBARDIER CL-600-2B16 Enhanced Surveillance Mode S Transponder Upgrade (Collins) N/A 15.03.2007 EASA.A.S.03156 REV 1 CESSNA 550 CITATION II Honeywell ART 2000 Weather Radar transceiver/antenna installation interfacing with KMD 850 MFD to replace the existing RCA P- 400 radar, to improve reliability and to add display of terrain and traffic graphics. 22.01.2008 EASA.A.S.03157 REV 1 CESSNA 550 CITATION II Honeywell EGPWS Mark VIII Sysem Installation,interfacing with KMD 850 MFD, as a replacement of the existing GPWS MK VI. 22.01.2008 EASA.A.S.03163 BEECH 200 Upgrade of dual Mode S transponder system TDR-94 to TDR-94D with ELS capability and diversity This change is limited to the configuration of aircraft / equipment type as listed under “1.2. Prerequisite Conditions”, in Engineering Order, Doc. No. 677-062, Initial Revision, dated 12- Jun-2007 EASA.A.S.03173 BOMBARDIER CL-600-2B16 Replacement of 3 FMS GPS Antennas (UASC) 04.09.2007 EASA.A.S.03187 BAE 125 -800A SERIES Upgrade of EGPWS MK V to RAAS capability. This STC is limited to the configuration of 10.01.2008 BAE 125-800B SERIES aircraft / equipment type as listed under Item 2.1 Limitation, in Engineering Order, Doc. No. 687- 062, Revision B, dated 18-Dec-2007, or later approved revision. EASA.A.S.03230 BAE 125 -800 SERIES Modification of Collins Transponders to achieve None. Enhanced Surveillance Capability. 10.09.2007 EASA.A.S.03333 BOMBARDIER CL-600-2B19 Dual Electronic Flight Bag Installation (Maxware). Aircraft Flight Manual Supplement 667-071. 11.04.2008 04/01/2013 Page 97/462 14.08.2007
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04/01/2013 Page 1/462 - EASA

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