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 10028304 KNOTS 2U, LTD. P- PA-28-151, PA-28-161, Piper Wing Tips with Landing / Recognition None Prior to installation of this modification it 16.12.2009 EASA.IM.A.S.03267 PA-28-181, PA-28-201T, Lights must be determined thatthe PA-28-236, PA-28R-201 interrelationship between this modification PA-28-RT-201T, PA-32-301 and any other previouslyinstalled PA-28R-201T, PA-28RT-201, modification and/ or repair will introduce PA-32-301 T, PA-32R-301, no adverse effectupon the airworthiness PA-32R-301T of the product. 10031230 KNOTS 2U, LTD. LBA EMZ SA1221 FAA SA1217GL 1. PA-32-301FT, PA-32-301XTC 1. PA-32R-301(HP) 1. PA-32R-301T(TC) 2. PA-32-301, PA-32-301T 2. PA-32R-301, PA-32R-301(SP) 10031235 KNOTS 2U, LTD. FAA STC SA1521GL 1. PA-32-301FT, PA-32-301XTC 1. PA-32R-301(HP) 1. PA-32R-301T(TC) 2. PA-32-301, PA-32-301T 2. PA-32R-301, PA-32R-301(SP) Installation of wing root fairings in accordance with FAA STC SA1217GL(Revision of LBA EMZ 1221, issue 1, dated July 20, 2001). Installation of flaps, aileron, flap/fuselage and stabilator gap sealsin accordance with FAA STC SA1521GL. 10031236 KNOTS 2U, LTD. LBA EMZ SA1222 FAA SA1195GL 1. PA-32-301FT, PA-32-301XTC Installation of Flap Hinge Fairing seals in 1. PA-32R-301(HP) accordance with FAA STCSA1195GL 1. PA-32R-301T(TC) (Revision of LBA EMZ 1222, issue 1, dated 2. PA-32-260, PA-32-300 2. PA-32-301, PA-32-301T 2. PA-32R-300, PA-32RT-300 2. PA-32R-301(SP), PA-32S-300 2. PA-32R-301T(SP), PA-32R-300 2. PA-32RT-300T July 20, 2001). 10014885 KORFF LUFTFAHRT EASA.A.S.03113 GROB G 109 GROB G 109 B 10014470 KUERZI AVIONICS AG EASA.A.S.02531 LEARJET 60 Installation of SSFDR and MFDAUInstallation of a Honeywell Solide State Flight Data Recorder and Teledyne Mini Data Acquisition Unit in Learjet Model 60 Changes:- at the luggage compartment to be 1. Limted to S/N: 62192. This STC is used as basis for instruments,- additional cable approved only for the product configuration as routing in the wings- reinforced attachment defined in the approved design data referred to points at the lower side of both wings for under in the paragraphs "Description" and wing pots- reinforcements of the root tips- “Associated Technical Documentation”. operation with external loa Compatibility with other aircraft/engine con 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. 03.08.2010 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. 03.08.2010 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. 03.08.2010 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 10014482 KUERZI AVIONICS AG EASA.A.S.02545 CESSNA 340A Avionic Retrofit 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. 25.04.2006 10014569 KUERZI AVIONICS AG EASA.A.S.02673 BOMBARDIER DHC-6 SERIES 300 Installation of KMH-880, GPS-400 & KMD-850. Limited to S/N 0841. 13.04.2007 10014716 KUERZI AVIONICS AG EASA.A.S.02892 PILATUS PC-12/45 Honeywell GNS-XLS FMS InstallationBy installing a single GNS-XLS Flight Management System with GPS and DME sensor. HB-FPI S/N 551. Valid for this S/N only. 23.04.2007 10014806 KUERZI AVIONICS AG EASA.A.S.03010 PILATUS PC-12/47 HF 1050 & AFFS Installation by installing a new S/N 795 for initial installation.Approval valid for 22.03.2007 HF-1050 HF COM System with a PS440 HF Control Panel and a new F5K AFFS (Automated Flight Following System). S/N 795 and any other PC-12/47. 10014878 KUERZI AVIONICS AG EASA.A.S.03105 PIPER PA-31T Installation of Dual Mode-S XPDR & TASInstallation of- Dual Mode S Transponder GTX-330D with diversity antenna.- Traffic 10014945 KUERZI AVIONICS AG EASA.A.S.03205 CESSNA 340A Advisory System SKY497 Installation of a Traffic Advisory System:By installing a SKY497 Skywatch Traffic Advisory System with appropriate antenna. Traffic information will be displayed on existingsystems. Reg. HB-LNLS/N: 31T-8020083Valid for this S/N only 04/01/2013 Page 300/462 30.04.2007 11.12.2006 11.05.2007 28.08.2007
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10014974 KUERZI AVIONICS AG EASA.A.S.03260 PILATUS PC-12/47 FMS and DME installation:By installinga new GNS-XLS FMSa new DM-441B DME 26.11.2007 10015230 KUERZI AVIONICS AG EASA.A.S.03648 PILATUS PC-12/47E FDR and CVR Installation. 1. 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 i 31.10.2008 10015275 KUERZI AVIONICS AG EASA.A.S.03770 PILATUS PC-12/45 GPS 400W and GMA 347 InstallationRemoved Prior to installation of this modification the 02.03.2009 Equipment:- KLM 90B GPS- Existing GPS installer must determine that the Antenna- KMA 24H Audio PanelNew Installed interrelationship between this modification and Equipment- GPS 400W GPS- GA 35 any other previously installed modification will GPS/WAAS Antenna- GMA 347 Audio Panel introduce no adverse effect upon the airworthiness of the product. The install 10015277 KUERZI AVIONICS AG EASA.A.S.03789 PIPER PA-23-250 Dual GNS430W, GMA340, KN 63 1. Prior to installation of this modification the InstallationOut: Dual KX-155 COM/NAV installer must determine that the systems, Trimble-2000 approach GPS system, interrelationship between this modification and KMA-24H Audio system, MKR-101 marker any other previously installed modification will system, KN-65 DME systemIn: Dual GNS- introduce no adverse effect upon the 430W system, GMA-340 Audio/MKR system, KN-63 DME system. airworthiness of the product.2. 10017221 KUERZI AVIONICS AG EASA.R.S.01382 BELL 206B Hellas installation:As a convertible EADS Reg.: D-HEDB S/N: 4197Valid for this S/N HELLAS (Helicopter Laser Radar) System that only provides the following functions:-Raw data acquisition-System development-System demonstrationThe rotorcraft can be operated either in a "Normal" or a "HELLAS" configurat 10017239 KUERZI AVIONICS AG EASA.R.S.01425 EUROCOPTER FRANCE SA 315B NVIS Conversion.Includes Rad. Altimeter and Mode S ELS Transponder installation. 10017262 KUERZI AVIONICS AG EASA.R.S.01471 BELL 206B Radar altimeter installation including adapter plate. 10027877 KUERZI AVIONICS AG P-EASA.A.S.03965 LEARJET 55 Installation of Satellite Tracking System SAT- 111 10033212 KUERZI AVIONICS AG 500N MD520N Gyro camera & equipment inst.(Gyrocam "Turret Assy" for filming or live broadcasting) 08.04.2009 25.10.2007 Reg.: HB-XII S/N: 2551Mode S Transponder system alleviation of flight status according JAA TGL-13 note 10 granted. 06.08.2008 1. 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 i 18.12.2008 None None 11.11.2009 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. 04.01.2011 10033622 KUERZI AVIONICS AG AS 350 B2, AS 350 B3 G500H Avionic Retrofit (Option 1 & 2)Option 1 None Prior to installation of this modification it 31.01.2011 Out: Original OEM installed -Airspeed Indicator - must be determined thatthe Gyro Horizon -Altimeter -Turn & Bank Indicator - interrelationship between this modification Directional Gyro -Vertical Speed Indicator In: - and any other previouslyinstalled Garmin G500H system including PFD/MFD modification and/ or repair will introduce GDU 620-Attitude heading Re no adverse effectupon the airworthiness of the product. As a m 10034392 KUERZI AVIONICS AG MYSTÈRE-FALCON 50 FMS upgradeUpdate of the existing UNS-1k to UNS-1LW. Installation of a second FMS.Upgrade of the existing Collins VIR-31 #1/2 and DME-41 #1/2 to VIR-32and DME-42 so that ARINC429 can be used to interface with the dual FMS. 10035249 KUERZI AVIONICS AG PC-6-B2-H4 Cold weather operation package (230VAC or 110VAC)By installation of:- One TANIS TAS200 Battery Heater system- One TANIS TAS300 Turbine Preheat system- One Power receptacle in the cabin front right Restricted to MF50 S/N 183. 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. 31.03.2011 S/N: all The approval holder shall fulfill the obligations of Part 21, §21.A109.Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair 04/01/2013 Page 301/462 08.06.2011
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04/01/2013 Page 1/462 - EASA

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