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 10040868 SABENA TECHNICS BOD A320-214 Installation of SATCOM system This modification can be installed only Prior to installation of this modification it 31.07.2012 concurrently with themodifications approved must be determined thatthe under EASA STC 10040867 (EASA interrelationship between this modification project0010016700).This approval is limited and any other previouslyinstalled only to MSN 3164. modification and/ or repair will introduce no adverse effectupon the airworthiness of the product. 10014573 SABENA TECHNICS DNR EASA.A.S.02677 FOKKER F.28 MARK 0100 Fokker 100 VIP Cabin Maximum approved passenger capacity: 19Limited to serial numbers 11368, 11403, 11406.Refer to AFM Supplement. 10016732 SAGEM AVIONICS, INC EASA.IM.R.S.01056 REV. 4 FAA STC SR09263RC-D EC120B SFIM two-axis VFR Autopilot System (SAGEM PA85)Nota:,,- Original STC: FAA STC SR09263RC-D, amended 9 February, 2011- Existing EASA STC: 10016732 rev 3- Revision 4 incorporates 2 new configurations related to minor changeto the FAA STC. 10016737 SAGEM AVIONICS, INC EASA.IM.R.S.01061 SR09291RC-D EUROCOPTER FRANCE EC 130 B4 10027509 SAGEM AVIONICS, INC P- EASA.IM.R.S.01527 10029542 SANDEL AVIONICS, Inc. P- EASA.IM.A.S.02918 Original STC nbr: FAA STC SR09291RC-D, amended 06-Oct-2006Installation of a two-axis REV. 2 FAA STC SR09450RC EC120B VFR auto-pilot Original STC: FAA STC SR09450RC, amended 11-May-2009SAGEM Integrated Cockpit Display System (ICDS) FAA STC ST01930LA S550 Installation of Sandel Avionics SA4550 Primary Attitude Display andSandel Avionics SN4500 Primary Navigation Display. 10017096 SAS MAT AVIATION EASA.R.S.01017 EUROCOPTER FRANCE EC 120 B 10016404 SAVANNAH AIR CENTER, L.L.C. EASA.IM.A.S.02733 FAA STC ST03528AT BOMBARDIER BD-700-1A11 Installation, Complete Custom Interior, s/n 10016536 SAVANNAH AIR CENTER, L.L.C. EASA.IM.A.S.02913 FAA STC SA02683AT, CAA UK AAN GULFSTREAM IV Installation of L3 Communications Digital Flight Data Recorder With Teledyne Digital Flight Installation of FAA STC SR09450RC (EASA.IM.R.S.01527) is mandatory forconfigurations -01, -02of SAGEM Installation Drawing 120-1002Installation of FAA STC SR09450RC (EASA.IM.R.S.01527) is mandatory forconfigurations -03, -04 of SAGEM Installation Dra For night VFR operations, the helicopter must be fitted with a backupinstrument permitting attitude control, such as a standby attitudeindicator or a slip/skid indicator 03.07.2007 Prior to installation of this modification it 14.03.2011 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. 08.12.2006 Prior to installation of this modification it 24.11.2009 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 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. 30.03.2010 Upgraded Avionics configuration 1. Limited to aircraft EC120B s/n 1049, F- GRAE only2. 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 s 22.08.2005 9229 Configuration. Restricted to ASN 9229. 01.04.2008 Only approved for Aircraft manufactured before 18 August 2000 10028136 SAVANNAH AIR CENTER, L.L.C. FAA STC ST03818AT BOMBARDIER BD-700-1A10 Data Acquisition Unit. Complete Custom Aircraft Interior - ASN 9287. Restricted to ASN 9287 for a total of 15 passengers. 10031798 SAVANNAH AIR CENTER, L.L.C. FAA STC ST12210AT-T BD-700-1A10 Installation, Complete Custom Interior, ASN 9347 Configuration. 10032322 SAVANNAH AIR CENTER, L.L.C. REV. 1 FAA STC ST03881AT BD-700-1A10 Installation, Complete Custom Interior, S/N 9345 Configuration 03.06.2008 Prior to installation of this modification it 04.12.2009 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. Restricted to ASN 93471.Refer to the Prior to installation of this modification it 14.09.2010 Limitations sections of the required AFM must be determined thatthe Supplement andto the referenced interrelationship between this modification FCOMS.2.WLAN system is compatible only to and any other previouslyinstalled IEEE 802.11(b). modification and/ or repair will introduce no adverse effectupon the airworthiness of the product. Restricted to ASN 9345 and1. Refer to the Prior to installation of this modification it 29.03.2011 Limitations sections of the required AFM must be determined thatthe Supplement andto the following interrelationship between this modification FCOMS:G862081 Rev NC - FCOMS - WLAN and any other previouslyinstalled SystemG862092 Rev A - FCOMS - Mid-Cabin modification and/ or repair will introduce Door2. WLAN system is compatible only to no adverse effectupon the airworthiness IEEE 802.11(b) of the product. 04/01/2013 Page 390/462
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10032416 SAVANNAH AIR CENTER, L.L.C. FAA STC ST03628AT BD700-1A10 Installation, Complete Custom Interior, S/N Restricted to ASN 9260 and1. Refer to the Prior to installation of this modification it 04.11.2010 9260 Configuration Limitations sections of the required AFM must be determined thatthe Supplement andto the referenced FCOMS.2. interrelationship between this modification WLAN system is compatible only to IEEE and any other previouslyinstalled 802.11(b). modification and/ or repair will introduce no adverse effectupon the airworthiness of the product. 10014558 SCAI TECH EASA.A.S.02657 REV. 3 DR 300/108, DR 300/120 DR 300/125, DR 300/140 DR 300/180 R, DR 315, DR 340 DR 360, DR 380, DR 400/100 DR 400/120 D, DR 400/125 DR 400/120, DR 400/120 A DR 400/140, DR 400/140 B DR 400/160, DR 400/160 D DR 400/180 S, DR 400/NGL DR 400/180, DR 400/180 R SCAI-DR315_DR300-108, 120, 125, 140_DR340_DR360-FM-A,SCAI- DR380_DR300-180R-FM-A, SCAI-DR412-FM- B, SCAI-DR416-414-FM-B,SCAI-DR418-FM- B, SCAI-DR221_DR221B-FM-A.Extension of EASA.A.S.02657 to DR221 aircraft. 10034639 SCAI-TECH EASA.A.S.02943 F150L, F150M, FA150L, FA150M SCAI-CE150-FM-A Echappement accorde avec silencieux double flux. 10013928 SCANDINAVIAN AVIONICS A/S EASA.A.S.00239 REV. 1 BEECH 400A Installation of a EGPWS Mk. VIII system in accordance with the Engineering Order Doc.: 2017016-EO-02 Issue 2 or later EASA approvedrevision. None. Prior to installation of this modification the 23.10.2009 installer must determinethat the interrelationship between this modification and any otherpreviously installed modification will introduce no adverse effect uponthe airworthiness of the product. Limitation to aircraft equipped with engine TCM Prior to installation of this modification it 02.06.2009 0-200-A and propellerMcCauley must be determined thatthe 1A102/0CM6948. interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product. 1. AFM Supplement Document No. 2017016-AM-02 Issue 2 or later EASA approved revisions.2. Maintenance Requirements and Instruction for Continuous Airworthiness Doc. 2017016-CA-02. 10013944 SCANDINAVIAN AVIONICS A/S EASA.A.S.00384 BAE 125 SERIES 800B Installation of an Universal CVR-30B Cockpit 1. This STC is approved only for the product Voice Recorder in accordance with the configuration as defined in the approved design Engineering Order Doc: 2022468-EO-01, Issue data referred to in the paragraph "Description". 1 orlater EASA-approved Revisions. AFM Compatibility with other aircraft/engine Supplement Document No 2022468-AM-01 configurations shall be determined by the Issue 1 or later EASA-approved Revisions. Maintenance installer. 10013971 SCANDINAVIAN AVIONICS A/S EASA.A.S.00766 SAAB SF340A Installation of an ADF 2 Bendix King KDF 806 1. This STC is approved only for the product System. 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. 10013994 SCANDINAVIAN AVIONICS A/S EASA.A.S.01028 LEARJET 55 Installation of a Rockwell Collins ACAS 1. Certification Basis for this STC is CS 25 plus (TCASII) 4000 with dual Mode S Transponders JAA TGL No 8 and JAA TGL No 13 10013995 SCANDINAVIAN AVIONICS A/S EASA.A.S.01029 LEARJET 55 Installation of a L3 Digital Flight Data Recorder Certification Basis for this STC is CS 25 31.01.2005 10013997 SCANDINAVIAN AVIONICS A/S EASA.A.S.01032 LEARJET 55 Installation of a Honeywell EGPWS mark VIII Certification Basis for this STC is CS 25 plus (TAWS) JAA TGL No 12 "TAWS" 10014015 SCANDINAVIAN AVIONICS A/S EASA.A.S.01058 REV. 1 AMD/BA FALCON 10 Installation of Rockwell Collins TCAS-4000 incl. Dual Mode S Transponder TDR-94D in accordance with the Engineering Order Doc 2022256-EO-01 Issue 2 or later EASA approved revisions 10014016 SCANDINAVIAN AVIONICS A/S EASA.A.S.01059 REV. 1 AMD/BA FALCON 10 Installation of a Kannad 406 ELT in accordance with Engineering Order Doc 2022256-EO-03, Issue 1 or later EASA approved revisions 10014017 SCANDINAVIAN AVIONICS A/S EASA.A.S.01060 REV. 2 AMD/BA FALCON 10 Installation of a Multi Function Radar Display (MFRD) and EGPWS MK VIII in accordance with the Engineering Order Doc 2022874-EO- 01,Issue 2 or later EASA approved revisions 10014025 SCANDINAVIAN AVIONICS A/S EASA.A.S.01091 BEECH 200 BEECH 200C BEECH B200 BEECH B200C 10014026 SCANDINAVIAN AVIONICS A/S EASA.A.S.01092 BEECH 200 BEECH B200 Installation of a Universal TAWS system and related components. 15.02.2008 07.12.2004 08.06.2005 31.01.2005 31.01.2005 30.05.2005 14.05.2005 09.08.2007 04.01.2007 Installation of GPS TNL-2101 I/O APPR+ 11.02.2005 04/01/2013 Page 391/462
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04/01/2013 Page 1/462 - EASA

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