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 10014027 SCANDINAVIAN AVIONICS A/S EASA.A.S.01093 REV. 1 BEECH 1900 1. Installation of Dual Mode S Transponder For installations on or after 31-Jan-2007, this 05.02.2007 BEECH 200C MST-67A System with ELS capabilities change is limited to the configuration of aircraft BEECH 300 (installation prior to 31-Jan-2007)2. / equipment type as listed underItem 4. in BEECH 300LW Installation of Dual Mode S Transponder MST- Engineering Order, Doc. No. 2021128-EO-03, BEECH B200C 67A System with ELS and EHS capabilities Issue 5, or later approved issue: BEECH B300 BEECH B300C (installation on or after 31-Jan-2007) 10014028 SCANDINAVIAN AVIONICS A/S EASA.A.S.01094 BEECH 200 Installation of Multifunction Display MFD-640 & 11.02.2005 BEECH B200 RP 1008 10014036 SCANDINAVIAN AVIONICS A/S EASA.A.S.01109 CESSNA 525 Installation of Honeywell KMH 980 Multi- Hazard Awareness System including TCAS I and EGPWS (Class B). 11.04.2005 10014037 SCANDINAVIAN AVIONICS A/S EASA.A.S.01110 CESSNA 525 Installation of WX-500 Stormscope System 11.04.2005 10014038 SCANDINAVIAN AVIONICS A/S EASA.A.S.01111 CESSNA 525 Installation of Bendix/King KLN 94 GPS System. 11.04.2005 10014050 SCANDINAVIAN AVIONICS A/S EASA.A.S.01132 LEARJET 35 Installation of Honywell CAS 67A ACAS/TCAS Certification Basis: applicable requirements of 31.05.2005 LEARJET 35A II with dual MST-67A Mode S Transponder CS25 plus JAA TGLs No 8 and 13 1. 10014091 SCANDINAVIAN AVIONICS A/S EASA.A.S.01189 REV. 1 CESSNA 500 CESSNA 550 CESSNA 560 CESSNA S550 10014092 SCANDINAVIAN AVIONICS A/S EASA.A.S.01190 CESSNA 650 Installation of FreeFlight 2101 I/O APPROACH PLUS GPS Navigation System 10014093 SCANDINAVIAN AVIONICS A/S EASA.A.S.01191 CESSNA 650 Installation of Honeywell CAS 67A TCAS II System, including Dual MST 67A Mode S Transponders 10014095 SCANDINAVIAN AVIONICS A/S EASA.A.S.01193 BAE ATP Installation of Universal Terrain Awareness Warning System (TAWS) 10014096 SCANDINAVIAN AVIONICS A/S EASA.A.S.01194 Installation of Universal UNS-1L Flight Management System 10014111 SCANDINAVIAN AVIONICS A/S EASA.A.S.01216 BEECH 300 BEECH B300 10014150 SCANDINAVIAN AVIONICS A/S EASA.A.S.01270 BEECH 200 BEECH 300 BEECH B200 BEECH B300 10014151 SCANDINAVIAN AVIONICS A/S EASA.A.S.01271 BEECH 200 BEECH 300 BEECH B200 BEECH B300 Installation of Kannad 406 AF ELT 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. 07.04.2005 - 25.08.2005 - 25.08.2005 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. Installation of Honeywell CAS 67A ACAS/TCAS II with Dual MST-67A Mode S Transponder EGPWS Installation on Airbus A300/A310 Refer to AFM Supplement Ref. Dc113-0846 Rev B and to Maintenance Planning Document Supplement DC114-0846-00 rev A. Installation of Dual GTX 330D Mode S Transponder System. 10014162 SCANDINAVIAN AVIONICS A/S EASA.A.S.01294 BAE 125 -800 SERIES Installation of a Rockwell Collins TCAS 4000 with dual TDR-94D Mode S Transponder 10014199 SCANDINAVIAN AVIONICS A/S EASA.A.S.01349 REV. 1 BEECH 200 BEECH 300 BEECH 300LW BEECH B200 BEECH B300 Installation of TAWS ST3400 system.Revision of the AFM Supplement related to a Minor Change to EASA.A.S.01349.Installation of TAWS ST3400 system.Revision of the AFM Supplement related to a Minor Change to EASA.A.S.01349. 10014200 SCANDINAVIAN AVIONICS A/S EASA.A.S.01350 CESSNA 500 Installation of Honeywell KMH 880 Multi- Hazard Awareness System 10014226 SCANDINAVIAN AVIONICS A/S EASA.A.S.01389 CESSNA 300 SERIES CESSNA 400 SERIES 10014242 SCANDINAVIAN AVIONICS A/S EASA.A.S.01451 CESSNA 500 CESSNA 550 CESSNA S550 10014245 SCANDINAVIAN AVIONICS A/S EASA.A.S.01455 CESSNA 300 SERIES CESSNA 400 SERIES Installation of GNS 430A/530A COMM/NAV/GPS Systems Installation of GPS400 in center panel with GAD 42 adapter for roll steering 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 paragraph "Description". Compatibility with other aircraft/engine configurations shall be determined by the installer.This STC is approved onl 26.07.2005 26.07.2005 30.05.2005 28.04.2005 29.06.2005 26.07.2005 26.02.2007 This STC is approved only for the product 02.01.2006 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. none 20.09.2005 24.01.2006 Installation of GTX 330 Mode S Tansponder 20.09.2005 04/01/2013 Page 392/462
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10014295 SCANDINAVIAN AVIONICS A/S EASA.A.S.01537 BEECH 400A (HAWKER 400 XP) IInstallation of a Rockwell Collins TCAS 4000 with dual TDR-94D Transponder 15.11.2005 10014313 SCANDINAVIAN AVIONICS A/S EASA.A.S.01561 BEECH 400A (HAWKER 400 XP) Installation of a L3 Digital FDR and Teledyne FDAU 22.11.2005 10014333 SCANDINAVIAN AVIONICS A/S EASA.A.S.01587 LETECKE ZAVODY L 410 UVP- Installation of Honeywell CAS 67A TCAS II 22.02.2006 E20 including dual MST 67A Mode S Transponder 10014343 SCANDINAVIAN AVIONICS A/S EASA.A.S.01603 PIPER PA-34-200 PIPER PA-34-200T PIPER PA-34-220T Installation of KMD 850 Multi Function Display 03.04.2006 10014360 SCANDINAVIAN AVIONICS A/S EASA.A.S.01625 BEECH A36 Replacement of existing KI-525A HSI system with new KI-825 EHSI system 20.02.2006 10014406 SCANDINAVIAN AVIONICS A/S EASA.A.S.01701 BEECH A36 Title: GARMIN GNS 430/530 upgrade for GPS approachDescription: Upgrade of existing GNS 430/530 for GPS approach and installation of annunciator panel 13.02.2006 10014435 SCANDINAVIAN AVIONICS A/S EASA.A.S.02484 REV. 1 CESSNA 500, CITATION CESSNA 550 CITATION II CESSNA 560 (CITATION V) CESSNA S550, (CITIATION S/II) 10014455 SCANDINAVIAN AVIONICS A/S EASA.A.S.02509 BOMBARDIER SD-3-60-SHERPA BOMBARDIER SD-3-SHERPA 10014469 SCANDINAVIAN AVIONICS A/S EASA.A.S.02530 CESSNA 500, CITATION CESSNA 550 CITATION II CESSNA 560 (CITATION V) CESSNA S550, (CITIATION S/II) 10014489 SCANDINAVIAN AVIONICS A/S EASA.A.S.02551 LEARJET 35 LEARJET 35A 10014496 SCANDINAVIAN AVIONICS A/S EASA.A.S.02559 DORNIER DO 228-100 DORNIER DO 228-101 DORNIER DO 228-200 DORNIER DO 228-201 DORNIER DO 228-212 10014497 SCANDINAVIAN AVIONICS A/S EASA.A.S.02560 DORNIER DO 228-100 DORNIER DO 228-101 DORNIER DO 228-200 DORNIER DO 228-201 DORNIER DO 228-212 Sandel ST3400 TAWS Installation left hand and right hand Collins TCAS 4000 with dual TDR-94D Transponder Installation Certifications Basis of the Change: CS 25, additionally JAA Leaflet No. 12 (TAWS) Certification Basis of the Change: CS-25, additionally JAA leaflet No. 8 Rev. 2 (ACASII), JAA Leaflet No. 13 Rev. 1 (Mode S ELS) 02.04.2006 01.08.2006 Installation of a Garmin GNS 530A and a Honeywell Marker Beacon KR21, for EU basic RNAV operations None 13.06.2006 Installation of Dual Universal UNS-1E FMS in Certification Basis of the change: CS 25, 06.04.2006 Learjet 35/35A Amdt. 01 Sandel ST3400 TAWS installationInstallation of -- Class A TAWS/RMI Indicator in the right hand instrument panel with a remote Annunciator and Switching unit on the left hand instrument panel. Single 3" indicator is used to show compliance 22.06.2006 Installation of Honeywell CAS 67A ACAS II System incl. Dual Mode S XPDR 10014539 SCANDINAVIAN AVIONICS A/S EASA.A.S.02626 Universal TAWS Installation incl. MFD-640 Certification Basis of the Change: CS 25 Amendment 1, additionally JAA Leaflet No. 12 (TAWS) 10014540 SCANDINAVIAN AVIONICS A/S EASA.A.S.02627 Installation of Universal UNS-1L(-1K+) FMS Certification Basis of the Change: CS 25 Amendment 1, additionally JAA Leaflet No. 10 (Precision RNAV), AMC 20-4 (Basic RNAV), AMC 20-5 (GPS) 10014550 SCANDINAVIAN AVIONICS A/S EASA.A.S.02643 CESSNA 501, CITIATION CESSNA 551, CITIATIONII 10014551 SCANDINAVIAN AVIONICS A/S EASA.A.S.02644 CESSNA 500, CITATION CESSNA 550 CITATION II CESSNA S550 (CITATION II) Installation of Dual Garmin GNS 430A/530A 1. Certification basis of the Change CS-23, and 3rd COMM in Cessna Citation I model 501 additionally:2. AMC 20-4 (Basic RNAV), and Citation II model 551. AMC 20-5 (GPS), AMC 25-11 (Electronic Display Systems) and JAA TGL 7, rev.1 (VHF Com 8.33 KHz).3. Prior to installation of this modification the installer must dete Installation of Dual Garmin GNS 430A/530A 1. Certification Basis of the Change CS-25 and 3rd COMM in Cessna Citation I model 500 Amdt. 2, additionally:2. AMC 20-4 (Basic and Citation II model 550, S550. RNAV), AMC 20-5 (GPS), AMC 25-11 (Electronic Display Systems) and JAA TGL 7, rev.1 (VHF Com 8.33 KHz)3. Prior to installation of this modification the installer mu 10014556 SCANDINAVIAN AVIONICS A/S EASA.A.S.02654 Honeywell EGPWS MK VI Installation Certification Basis of the Change CS 25, additionally JAA TGL 12 (TAWS) 10014559 SCANDINAVIAN AVIONICS A/S EASA.A.S.02658 Trimble TNL-2101 I/O Aproach + GPS System Certification Basis of the Change CS 25, Installation additionally EASA AMC 20-4 (BRNAV) and AMC 20-5 (GPS) 10014582 SCANDINAVIAN AVIONICS A/S EASA.A.S.02688 BAE 125 -800 SERIES Installation of an In-flight Entertainment System This change is limited to airplanes equipped HAWKER 800 HAWKER 800 XP with ARINC 429 Interface to GPS / FMS 10014592 SCANDINAVIAN AVIONICS A/S EASA.A.S.02703 BAE JETSTREAM 3100 Sandel ST3400 TAWS installation Certification Basis of the Change CS 25, BAE JETSTREAM 3200 additionally JAA TGL No. 12 (TAWS) 04/01/2013 Page 393/462 12.06.2006 27.06.2006 27.06.2006 20.06.2007 20.06.2007 06.06.2006 06.06.2006 22.03.2007 21.07.2006
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04/01/2013 Page 1/462 - EASA

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