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 10014889 RUAG AEROSPACE SERVICES GmbH EASA.A.S.03119 DORNIER 328-300 Modification of rear-facing seat for use during T/O and Landing.Backrest support of the already certified VIP seats AMP 2524..xxx is modified. The seats are now certified for T/O and landing in aft facing condition with a backrest support; ref. TSO-C127 dy 19.11.2007 10014890 RUAG AEROSPACE SERVICES GmbH EASA.A.S.03120 DORNIER 328-300 EASA Certification of Installed of Galley and Lavatory Water System.Certified earlier by AvCraft USA.Ref. FAA STC nr. 9993. 13.11.2007 10014891 RUAG AEROSPACE SERVICES GmbH EASA.A.S.03121 BOMBARDIER CL-600-2A12 (CL- EASA recertification of Cabin Modifications 601 29.02.2008 10014892 RUAG AEROSPACE SERVICES GmbH EASA.A.S.03122 BOMBARDIER CL-600-2A12 (CL- EASA recertification of Avionics Modification 601 29.02.2008 10014895 RUAG AEROSPACE SERVICES GmbH EASA.A.S.03125 DORNIER 228-212 Adjustment of Special Fatigue Life.Model: Dornier 228-212, S/N 8181 and 8183 10014935 RUAG AEROSPACE SERVICES GmbH EASA.A.S.03190 BOMBARDIER CL-600-2B16 (601- Installation of a Honeywell Bendix/King Radio 3A KTR 909 System. 10014938 RUAG AEROSPACE SERVICES GmbH EASA.A.S.03195 BOMBARDIER CL-600-1A11 (CL- Aircell Iridium Satcom, Axxcess EZ (Magnaster 600 BOMBARDIER CL-601-3A C-2000 replacement). 10014954 RUAG AEROSPACE SERVICES GmbH EASA.A.S.03219 CESSNA 650 CITATION III Honeywell EGPWS Mk VIIDescription: CESSNA 650 CITATION VI replacement of the existing GPWS Mk VII with CESSNA 650 CITATION VII a Honeywell EGPWS Mk VII. Terrain presentation on the EFIS MFD.Installation of indicators/switches in the instremental Panel. 1. This STC is only applicable to aircraft S/N: 08.10.2007 8181, 8183.2. Prior to installation of this modification the installer must determine that the interrelationship between this modification and any other previously installed modification will introduce Restricted to ASN 5105. 10.10.2007 10014964 RUAG AEROSPACE SERVICES GmbH EASA.A.S.03236 BEECH F90 Avionics Installation, consisting of- Dual GNS430A VHF Com/GPS and NAV- Dual GAD42 Adapter for GNS430/RMI- Dual KMR675 Marker Beacon Receiver- EHS GTX330D Diversity Transponder and Transponder Top Antenna- GMX200 Traffic/Radar and Jeppview MFD Display- TAS None. 12.12.2007 10014995 RUAG AEROSPACE SERVICES GmbH EASA.A.S.03292 Installation of dual Garmin GBS530AW Vertical approach navigation basing on NAV/COMM/GPS and dual sandel SN4500 E- GPS/WAAS is o nly approved in HS. VMC.Restricted to aircraft equipeed with Honeywell King Silver Crown Series. 10015005 RUAG AEROSPACE SERVICES GmbH EASA.A.S.03305 CESSNA 650 CITATION III CESSNA 650 CITATION VI CESSNA 650 CITATION VII 10015041 RUAG AEROSPACE SERVICES GmbH EASA.A.S.03357 CESSNA 525 CESSNA 525A FMS Upgrade to Dual Honeywell NZ- 2000/PRNAV Iridium Satcom AirCell ST3100,Description: Replacement to the previously installed AirCell AT.01 Air Telephone System by AirCell ST 3100 satellite Communication System (SATCOM). 21.08.2007 08.10.2007 17.03.2008 none 16.01.2008 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 10015054 RUAG AEROSPACE SERVICES GmbH EASA.A.S.03375 DORNIER DO 228-202K Increase of Fatigue Life Limit. This STC is only applicable to Aircraft S/N: 8046. 19.12.2007 10015094 RUAG AEROSPACE SERVICES GmbH EASA.A.S.03431 BEECH B200 Dual Collins TDR-94() Upgrade-ELS/EHS and None Antenna Diversity.Upgrade of existing Dual Collins TDR-94() Transponders by TDR-94D and Replacement of Control CTL-92 by CTL- 92E.Installation of two additional top-mounted L-Band Antennas for antenna diversity.Inst 08.02.2008 10015124 RUAG AEROSPACE SERVICES GmbH EASA.A.S.03474 REV. 1 FALCON 20 Dual Universal UNS-1L FMS Installation. This STC is limited to Mystere-Falcon 20-C5 aircraft Serial Number 141.See: Airplane Flight Manual Supplement 236A-F20-34.60.02AFMS Revision N/CMaintenance Manual Supplement 236A-F20-34.60.02MMS Revision N/COr later approved revisions. 10015125 RUAG AEROSPACE SERVICES GmbH EASA.A.S.03475 REV. 1 FALCON 20 Dual Collins TDR-94D Enhanced Mode S Transponder Upgrade. This STC is limited to Mystere-Falcon 20-C5 aircraft Serial Number 141.See:Airplane Flight Manual Supplement 236B-F20-34.80.05AFMS Revision OriginalOr later approved revisions. 04/01/2013 Page 380/462 08.02.2008 01.04.2008 31.03.2008
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10015259 RUAG AEROSPACE SERVICES GmbH EASA.A.S.03713 REV. 1 DC-9-87 (MD-87) Cabin Layout ChangeModification of existing 1. Prior to installation of this modification the 02.12.2008 Iberia 109 passenger economy seat layout to- installer must determine that the 20 B/C + 79 E/C seat layout for S/N 49832; interrelationship between this modification and 49834;49837; 49838; 49840; 49841 and- 12 any other previously installed modification will B/C + 89 E/C seat layout for S/N 49833; introduce no adverse effect upon the 49839; 49842 airworthiness of the product.2. 10015306 RUAG AEROSPACE SERVICES GmbH EASA.A.S.03897 EMBRAER EMB-135BJ Stone Flooring / Replacement of existing floor EASA EWIS Generic Special Condition not 26.05.2009 covering by a stone floor covering in the forward entrance area and in the rear lavatory. This modification will not affect the structural flooring, the stone floor covering is only a decorative component. applicable for this STC 10027158 RUAG AEROSPACE SERVICES GmbH P-EASA.A.S.03970 CESSNA 525 P-RNAV Upgrade for the Honeywell GNS-XLS Restricted to aircraft with S/N 0001 to 0359 1) Prior to installation of this modification 10.09.2009 Flight Management System 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 10027192 RUAG AEROSPACE SERVICES GmbH P-EASA.A.S.03963 BD-700-1A10, -1A11 EGPWS MK V Enhancement with RAAS - BD-700-1A10: S/N 9002 and subsequent- BD-Prior to installation of this modification it 14.09.2009 Upgrade of the existing Honeywell Enhanced 700-1A11: S/N 9127 and subsequent must be determined thatthe Ground Proximity WarningSystem (EGPWS) interrelationship between this modification MK V with the Honeywell Runway Awareness and any other previouslyinstalled and AdvisorySystem (RAAS). Installation of an modification and/ or repair will introduce optional RAAS Advisory Mute switchinto the no adverse effectupon the airworthiness center pede of the product. 10027824 RUAG AEROSPACE SERVICES GmbH CL-600-2B16 Installation of Honeywell Aircraft Flight Information System (AFIS) 10028151 RUAG AEROSPACE SERVICES GmbH REV. 1 EMB-135BJ AXE4-869/2009-mk (297A-RFC): Electronic Flight Bag 10030045 RUAG AEROSPACE SERVICES GmbH CL-600-1A11 / -2A12 / -2B16 EASA AD 2009-0097 and AD 2009-0173 for Transponder TDR-94D 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. 09.11.2009 None. EMB-135 model BJ not affected by EWIS requirements.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 30.06.2010 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. 17.05.2010 10030478 RUAG AEROSPACE SERVICES GmbH BD-700-1A11 Stone Flooring 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. 17.06.2010 10031258 RUAG AEROSPACE SERVICES GmbH DC-9-83 (MD 83) Cabin Layout/Interior Change -DC-9-83 none Refer to RUAG Doc. No. 293B- AMMSPrior 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 airwo 04/01/2013 Page 381/462 05.08.2010
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04/01/2013 Page 1/462 - EASA

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