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 10014605 SCANDINAVIAN AVIONICS A/S EASA.A.S.02728 CESSNA 650 CITATION III Installation of Honeywell Multi-Function Radar This STC is only applicable to Aircraft without 11.09.2006 CESSNA 650 CITATION VI Display (MFRD) and as an option a Honeywell EFIS system and integrated MFD. Primus 400 Radar system. 10014622 SCANDINAVIAN AVIONICS A/S EASA.A.S.02756 CESSNA 500, CITATION Installation of a “Flight Display Systems” The IFE sound shall be overrided by the PA 31.08.2006 CESSNA 550 CITATION II Entertainment System: DVD player, Map system CESSNA 560 (CITATION V) CESSNA S550 (CITATION II) computer and 2 LCD displays 10014632 SCANDINAVIAN AVIONICS A/S EASA.A.S.02774 BEECH 60 Installation of Mode S Transponder Garmin 11.10.2007 BEECH A60 BEECH B60 GTX 330D 10014641 SCANDINAVIAN AVIONICS A/S EASA.A.S.02791 CESSNA 550 BRAVO Honeywell EGPWS MK VIII Installation Certification Basis of the Change: CS 25 03.11.2006 CESSNA 560 Amanedment 1m, aditionally JAA Leaflet No. 12 (TAWS) 10014668 SCANDINAVIAN AVIONICS A/S EASA.A.S.02826 Honeywell EGPWS MK VI 1. This STC is only applicable for aircraft 30.01.2007 Installation.Installation of Honeywell Enhanced which have all the following equipment already Ground Proximity Warning System installed:Honeywell (Bendix-King) IN-182 EGPWS/TAWS. or KMD-850 Radar DisplayKN-53 NAV SystemKRA-405 Radar AltimeterKCS-55A Compass SystemComputer Instruments Corp. 10014672 SCANDINAVIAN AVIONICS A/S EASA.A.S.02832 BAE 125 -800 SERIES HAWKER 800 HAWKER HS 125-600 SERIES HAWKER HS 125-700 SERIES 10014673 SCANDINAVIAN AVIONICS A/S EASA.A.S.02833 BAE 125 -800 SERIES HAWKER 800 HAWKER HS 125-600 SERIES HAWKER HS 125-700 SERIES 10014689 SCANDINAVIAN AVIONICS A/S EASA.A.S.02852 BOEING 707-300 BOEING 737-400 BOEING 737-500 Installation of a Universal Terrain Awareness Warning System (TAWS). Installation of a Universal UNS-1F and / or UNS-1L Flight Management System for Basic RNAV, Precision RNAV Operations and Nonprecision Approaches and also as a primary means of navigation for oceanic/remote operations. Transponder S Mode Elementary and Enhanced Surveillance / Upgrade of existing dual diversity Transponder Mode S Installation 1. This change is limited to following configuration of the aircraft / equipment type:all airplanes equipped with* ARINC 429 Air Data Computers with temperature compensation, and * Rockwell Collins Proline 2 or 4 RADALT, VOR/ILS, and* Display S 1. This change is limited to following configuration of the aircraft / equipment type:all airplanes equipped with* Rockwell Collins Proline 1 (only NAV receiver), Proline 2 or 4 Navigation Equipment,and * Rockwell Collins analog HSI’s or EFIS 85/8 Certification Basis of the change: CS 25 Amdt. 2, additionally JAA TGL 13 Rev. 1 (Mode S ELS), JAA TGL 18 (Mode S EHS, compliance to JAA NPA 20-12a shown voluntarily.This STC is approved only for the product configuration as defined in the approved design 10014690 SCANDINAVIAN AVIONICS A/S EASA.A.S.02853 CESSNA 650 Honeywell EGPWS MK VIII Installation Certification Basis of the Change: CS 25 Amendment 2, additionally JAA Leaflet No. 12 (TAWS). 10014695 SCANDINAVIAN AVIONICS A/S EASA.A.S.02861 BAE 125 -800 SERIES HAWKER 800 10014702 SCANDINAVIAN AVIONICS A/S EASA.A.S.02872 REV. 2 HAWKER 800 HAWKER 800 XP HAWKER HS 125-700 SERIES 10014703 SCANDINAVIAN AVIONICS A/S EASA.A.S.02874 FAIRCHILD SWEARINGEN SA 226-TC FAIRCHILD SWEARINGEN SA 227 FAIRCHILD SWEARINGEN SA 227-AC FAIRCHILD SWEARINGEN SA 227-BC 10014729 SCANDINAVIAN AVIONICS A/S EASA.A.S.02907 REV. 1 CESSNA 500, CITATION CESSNA 550 BRAVO CESSNA 550 CITATION II CESSNA 560 (CITATION V) 10014759 SCANDINAVIAN AVIONICS A/S EASA.A.S.02948 CESSNA 650 CITATION III CESSNA 650 CITATION VI CESSNA 650 CITATION VII Installation of a Honeywell Class A Enhanced Ground Proximity Warning System EGPWS/TWAS for aircrafts equipped with a compatible MFD or weather radar display. Mode S Transponder Upgrade for existing Collins transponder system. 1. This change is limited to following configuration of the aircraft / equipment type:* Rockwell Collins EFIS 85/86 with ARINC 453 interface, and* Airdata system with ARINC 429 interface (TSO-C10b or C106), and* Rockwell Collins VIR-432 with ARINC 1. This STC approves only the installation of the parts contained in the above section “Description of Type Design Change”. This STC grants no operational approval to this installation, that will need to be obtained from the State of registry for the parti Installation of a Garmin GPS 400 System with This change is limited to following configuration Remote Annunciator Switch Panel in Fairchild of the aircraft / equipment type:-Airdata system Swearingen SA226-TC, SA227-AC, SA227 BC must be either ARINC 429, RS232 or Grey code as defined in the GPS 400 installation manual, and- any model of Rockwell Collins VIR-30/31/32 VOR/ILS Mode-S upgrade for existing Honeywell MST 67A transponder system. Upgrade of existing MST-67A Transponder System 10.01.2007 10.01.2007 03.01.2007 13.02.2007 03.01.2007 06.03.2007 14.12.2006 N/A 03.04.2007 As defined in Scandinavian Avionics Modification ref 2036080. 04/01/2013 Page 394/462 12.02.2007
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10014763 SCANDINAVIAN AVIONICS A/S EASA.A.S.02953 CESSNA 425 Replacement of one existing Transponder This change is limited to the configuration of 11.05.2007 System by a Garmin GTX 330D Mode-S aircraft / equipment type as listed under Item 4. Transponder System in Engineering Order, Doc. No. 2037527-EO, Issue 3, dated 04-May-2007 or later approved issuePrior to installation of this modification the installer must dete 10014767 SCANDINAVIAN AVIONICS A/S EASA.A.S.02959 CESSNA 500, CITATION Installation of Honeywell Multi-Function Radar 1. Prior to installation of this modification the 16.02.2009 CESSNA 550 CITATION II (MFRD) and an optional Honeywell Primus installer must determine that the CESSNA S550, (CITIATION S/II) Radar System, if the existing radar is interrelationship between this modification and incompatible with the MFRD. any other previously installed modification will introduce no adverse effect upon the airworthiness of the product.2. 10014777 SCANDINAVIAN AVIONICS A/S EASA.A.S.02975 CESSNA 650 CITATION III Installation of Honeywell TRA-45A Terrain Aircraft Serial No. 650-0037 with FOCA STC 29.05.2007 CESSNA 650 CITATION VI Display/ Radio Altimeter Indicator. Z34-44-05 installed as defined in Scandinavian CESSNA 650 CITATION VII Avionics Modification Reference 2037690. 10014778 SCANDINAVIAN AVIONICS A/S EASA.A.S.02976 CESSNA 650 CITATION III CESSNA 650 CITATION VI CESSNA 650 CITATION VII 10014800 SCANDINAVIAN AVIONICS A/S EASA.A.S.03003 SAAB 340B SAAB SF340A 10014807 SCANDINAVIAN AVIONICS A/S EASA.A.S.03011 CESSNA 501, CITIATION CESSNA 551, CITIATIONII 10014809 SCANDINAVIAN AVIONICS A/S EASA.A.S.03013 BEECH 200 BEECH 200C BEECH 300 BEECH 300LW BEECH B300 BEECH B300C 10014823 SCANDINAVIAN AVIONICS A/S EASA.A.S.03036 CESSNA 500, CITATION Installation of a single diversity Mode-S transponderGarmin GTX 330D and a new top antenna. 10014879 SCANDINAVIAN AVIONICS A/S EASA.A.S.03107 REV. 1 CESSNA 650 CITATION III CESSNA 650 CITATION VI CESSNA 650 CITATION VII 10014910 SCANDINAVIAN AVIONICS A/S EASA.A.S.03154 LEARJET 31 LEARJET 31A LEARJET 35 LEARJET 35A LEARJET 36 LEARJET 36A 10014957 SCANDINAVIAN AVIONICS A/S EASA.A.S.03227 REV. 1 DC-9-10 SERIES DC-9-20 SERIES DC-9-30 SERIES DC-9-40 SERIES DC-9-50 SERIES DC-9-81 (MD-81) DC-9-82 DC-9-83 DC-9-87 (MD-87) MD-88 MD-90 10014965 SCANDINAVIAN AVIONICS A/S EASA.A.S.03238 CESSNA 501 CESSNA 551 10015008 SCANDINAVIAN AVIONICS A/S EASA.A.S.03308 CESSNA 500, CITATION CESSNA 550 CITATION II CESSNA S550 (CITATION II) Installation of Sandel ST3400 TAWS System. 04.04.2007 Installation of Universal UNS-1L/K+, FMSsystem. N/A 13.04.2007 Installation of a Honeywell CAS 67A ACAS II This change is limited to the configuration of 03.04.2007 System and a Dual MST 67A Mode S aircraft / equipment type as listed under Item 4. Transponder System in Engineering Order, Doc. No. 2038224-EO, Issue 2, dated 21-Mar-2007 or later approved issue. Installation of Universal UNS-1L (-1K+) FMS This change is limited to the configuration of aircraft / equipment type as listed under Item 4. in Engineering Order, Doc. No. 2037417-EO, Issue 2, dated 09-Feb-2007 or later approved issue. 13.02.2007 Mode S Upgrade of existing Honeywell Transponder System RCZ-833 to comply with ICAO requirements for Mode S ELS and EHS.Minor change to EASA.A.S.03107:AFM Supplements for different Downlinked Aircraft Parameters.Mode S Upgrade of existing Honeywell Transpo Installation of a SANDEL ST3400 TAWS System (Class A) Mode S elementary and enhanced Upgrade of existing dual transponder system. Dual installation of Transponder Mode S System, MST 67A with PS 550 or PS 578A Mode S Control Panel, with ELS and EHS capability. Installation of Honeywell GNS-XLS FMS and L3 Standby horizon Reference System. According to EUROCONTROL definition this equipment with approval EASA.A.S.03036 is non-EHS compliant.Prior to installation of this modification the installer must determine that the interrelationship between this modification and any other previously insta As defined in Scandinavian Avionics Modification ref 2037689.As defined in Scandinavian Avionics Modification ref 2037689. Previous required aircraft configuration:All models equipped with:• Compatible Air Data Computers with ARINC 429 interface, and• Analogue Radio Altimeter interface (except ARINC 552) such asRockwell Collins ALT- 50/50A , ALT-55 or Honeywell RT-200/300, and\ Prior to installation of this modification the 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 This change is limited to the configuration of aircraft / equipment type as listed under Item 4. in EASA approved Engineering Order, Doc. No. 2041564-EO, Issue 2, dated 13-Aug-2007 or later approved issue 04/01/2013 Page 395/462 06.06.2007 20.11.2007 22.02.2008 24.07.2008 26.09.2007 28.11.2007
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04/01/2013 Page 1/462 - EASA

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