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 10014973 SCANDINAVIAN AVIONICS DESIGN EASA.A.S.03259 REV. 5 737-300, -400, -500, -600 Installation of a Dual navAero Electronic and Not Applicable Prior to installation of this modification it 14.11.2011 GMBH 737-700, -800, -900 logging display system.Change consisting in must be determined thatthe installing a dual portable Class 2 EFB's interrelationship between this modification t.BagC2system and any other previouslyinstalled modification and / or repair will introduce no adverse effectupon the airworthiness of the product. 10015305 SCANDINAVIAN AVIONICS DESIGN GMBH 10026864 SCANDINAVIAN AVIONICS DESIGN GMBH 10027014 SCANDINAVIAN AVIONICS DESIGN GMBH 10028068 SCANDINAVIAN AVIONICS DESIGN GMBH 10028206 SCANDINAVIAN AVIONICS DESIGN GMBH 10028452 SCANDINAVIAN AVIONICS DESIGN GMBH 10031128 SCANDINAVIAN AVIONICS DESIGN GMBH 10031822 SCANDINAVIAN AVIONICS DESIGN GMBH EASA.A.S.03894 REV. 1 1. 200, 200C, 300, 300LW 2. B200, B200C, B300, B300C P-EASA.A.S.03938 REV. 1 CESSNA 500, 550 GARMIN GPS 400W/500W installation Revision 1 supersedes the previous issue of this STC to delete the modelS550 from the applicability list for correction. P-EASA.A.S.03849 500 (CITATION AND CITATION I) Installation of Honeywell MST 67A Dual Mode S XPDR transponder. Dual TDR-94D Mode S ELS/EHS Transponder This change is limited to the configuration of System Upgrade, and optional forADS-B aircraft / equipment typeas listed under Chapter 4. in EASA approved Engineering Order, Doc. No.2073065-EO, Issue 1, dated 22-Mar-2012, or later approved issue forinstallations without ADS-B, or Issue 2, dated P-EASA.A.S.03732 650 (CITATION VII) Software upgrade of installed Honeywell GNS- XL or GNX-XLS FMS system forP-RNAV operation P-EASA.R.S.01586 R22 BETA Title: Camera with supportDescription: Optional Installation of a camera turret, related recorderand data link transmitter system in accordance with Master Document List2053852 DOC issue 2, dated 04.12.2009. The installation is based onScandinavian Avionic P-EASA.R.S.01580 REV. 1 EC 120 B Replacement of existing SAFT Ni-Cad. battery with Concorde lead acidbattery RG-350.Note: this STC is issued for the purpose of transfering STC No. 10028452from Airalpha A/S (DOA 21J.268) to new STC holder Scandinavian AvionicsDesign GmbH (DOA 21J.014) EASA.R.S.01449 EUROCOPTER FRANCE AS 365N EUROCOPTER FRANCE AS 365N1 EUROCOPTER FRANCE AS 365N2 EUROCOPTER FRANCE AS 365N3 ATR 42-200/300/320 Installation of Rockwell Collins TCAS-94 System with Single TDR-94DSystem, as per Scandinavian Avionics Engineering Order 2056096-EO issue1 dated 27th September 2010 or later EASA approved revisions. The limitations according to Aircraft Flight Manual Supplement2054628-AM are applicable. The installation of this modification by third persons is subject towritten permission of the approval holder and disposal of the approvedappropriate documentation.Prior to installation of this modification it must be determined thatthe interrelationship b 30.03.2012 1) Prior to installation of this modification 18.08.2009 the installer mustdetermine that the interrelationship between this modification and anyother previously installed modification will introduce no adverse effectupon the airworthiness of the product. 2) The inst None 1. Prior to installation of this modification 31.08.2009 the installer mustdetermine that the interrelationship between this modification and anyother previously installed modification will introduce no adverse effectupon the airworthiness of the product.2. The insta Limited to: S/N 650-7001 thru 650-7119 This Prior to installation of this modification it 30.11.2009 STC applies only for Single or Dual FMS GNS- must be determined thatthe XL or GNS-XLSconfiguration, approved for B- interrelationship between this modification RNAV operation. Intermixing with other FMSis and any other previouslyinstalled not approved within this STC. modification and/ or repair will introduce no adverse effectupon the airworthiness of the product. - S/N 0501 and subsequent,,- Pitot heat and Search Light must not be installed,, Not Applicable 10.12.2009 None The approval holder shall fulfill the obligations of Part 21, Paragraph21A.118A.The installation of this modification by third persons is subject towritten permission of the approval holder.Prior to installation of this modification the installer must be 12.12.2012 None No additional EWIS ICAS tasks over those already identified by theoriginal TC Holder for the applicable aircraft models are needed asconsequence of the implementation of this STC.Prior to installation of this modification it must be determined thatthe inte 11.10.2010 25.06.2009 04/01/2013 Page 398/462
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10031899 SCANDINAVIAN AVIONICS DESIGN HAWKER 800XP Installation of an International Communications Model Hawker 800XP, S/N: 258358 Prior to installation of this modification it 20.09.2010 GMBH Group Inc, ICS-100Iridium Satellite Telephone. 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. 10032285 SCANDINAVIAN AVIONICS DESIGN GMBH 10032445 SCANDINAVIAN AVIONICS DESIGN GMBH 10033395 SCANDINAVIAN AVIONICS DESIGN GMBH 10033781 SCANDINAVIAN AVIONICS DESIGN GMBH 10033782 SCANDINAVIAN AVIONICS DESIGN GMBH 10034415 SCANDINAVIAN AVIONICS DESIGN GMBH 10036450 SCANDINAVIAN AVIONICS DESIGN GMBH 10036673 SCANDINAVIAN AVIONICS DESIGN GMBH REV.1 CESSNA 500 CESSNA 550 CESSNA S550 P-EASA.A.S.03767 BEECH 1900C, AIRLINER BEECH 200 BEECH 200C BEECH 300 BEECH 300LW BEECH B200 BEECH B200C BEECH B300 BEECH B300C P-EASA.A.S.03768 200, 200C, B200 B200C, 300, 300LW, B300 B300C, 1900C SF340A AND 340B Installation of Collins TCAS-94 system with dual Collins TDR-94Dtransponders. SA226-T(B), SA227-AT, SA227-TT Installation of Garmin GNS 530AW / GNS SA26-AT, SA226-T, SA226-AT 430AW as dual installationtogether with a Honeywell KMR 675 Marker Beacon Receiver GPS / Navigation / Communication, Dual Garmin GNS 430/530 AWinstallationThe installation includes GPS antenna and single marker beacon receiver(KMR 675 or 51Z6) installation Installation of Sandel SA4550 EADI and Sandel SA4500 EHSI CollinsAHS-1000 Installation of Garmin GNS 430AW/GNS 530AW EASA.A.S.03858 BEECH 400, 400A Installation of various Entertainment Systems acc.: Engineering OrderDoc.: 2051195-EO Compliance Record Doc.: 2051195-COR P-EASA.A.S.03703 SD3-30, SD3-60 SD3-SHERPA, SD3-60 SHERPA GULFSTREAM 200 / GALAXY UPGRADE OF ROCKWELL COLLINS TDR- 94D MODE S TRANSPONDER SYSTEM FORENHANCED (EHS) SURVEILLANCE CAPABILITY. Transponder system NOT approved for ELS or Prior to installation of this modification it 22.10.2010 EHS. 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. This change is limited to the configuration of aircraft / equipment typeas listed under Chapter 4. in EASA approved Engineering Order, Doc. No.2061255-EO, issue 1, dated 26-Oct-2010, or later approved issue. The installation of this modification by third persons is subject towritten permission of the approval holder and disposal of the approvedappropriate documentation.Prior to installation of this modification it must be determined thatthe interrelationship b 08.11.2010 None - Directional Gyro or AHRS with synchro 21.01.2011 output (XYZ)- Analog HIS (RD044/RD650)/ADI (AD650) and RMI (332C)- Honeywell SPZ 500 AP/FD- One Receiver/Transmitter VHF-20B or VHF- 22x with CTL-22/20 or 313N-5A Control Panel- DME with 2*5 parallel DME tuning- Air This change is limited to the configuration of The installation of this modification by 01.07.2009 aircraft / equipment typeas listed under Item 4. third persons is subject towritten in EASA approved Engineering Order, Doc. permission of the approval holder, and No.2050691-EO, issue 1, dated 25-May-2009, having the appropriateapproved or later approved issue. documentation at one's disposal. Prior to installation of this modification it must be determined thatthe inte This change is limited to the configuration of The installation of this modification by 01.07.2009 aircraft / equipment typeas listed under Item 4. third persons is subject towritten in EASA approved Engineering Order, Doc. permission of the approval holder, and No.20S1374-EO, issue 1, dated 10-Jun-2009, having the appropriateapproved or later approved issue. documentation at one's disposal. Prior to installation of this modification it must be determined thatthe inte 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. 28.07.2009 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 09.09.2011 Installation of GARMIN GPS-400 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. 28.09.2011 04/01/2013 Page 399/462
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04/01/2013 Page 1/462 - EASA

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