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 10029701 CESKA LETECKA SERVISNI A.S. P-EASA.A.S.03951 SUKHOI SU-31 Avionics upgrade. None. Prior to installation of this modification the 14.04.2010 installer must determinethat the interrelationship between this modification and any otherpreviously installed modification will introduce no adverse effect uponthe airworthiness of the product. 10016012 CESSNA AIRCRAFT COMPANY EASA.IM.A.S.02178 ST01399WI CESSNA 560 Cessna STC ST01399WI, of 21 August 05.02.2007 CESSNA 650 CITATION III 2006.Installation of a Honeywell DL-950 Data CESSNA 650 CITATION VI CESSNA 650 CITATION VII CESSNA 750 CITATION X Loaderto replace the existing DL-800. 10016637 CESSNA AIRCRAFT COMPANY EASA.IM.A.S.03077 FAA STC SA01519WI CESSNA 525 Installation of an observer seat/3rd audio 1. Prior to installation of this modification the 28.11.2008 station/Extended Range Comm. 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.2. 10013934 CESSNA CITATION EUROPEAN EASA.A.S.00334 REV. 1 CESSNA 525 Installation of a Skywatch HP SKY899A TCAS 1. Applicability: Cessna 525 MSN 525-001 to 30.08.2007 SERVICE I coupled to a Honeywell KMD-850 MFD, in 359 included equipped with Honeywell WX RSaccordance with Cessna Citation European Service Center FAM Ref.: 111, Rev NC. Dated 14 August 2007 and FAM ref 82, Rev 01, dated 22 October 2004 or later approved revision 811A and FMS GNS-XLS. 10016805 CHELTON FLIGHT SYSTEMS EASA.IM.R.S.01165 REV. 1 FAA STC SR02209AK BELL 206A Installation of FlightLogic Synthetic Vision EFIS/AIU integration with the autopilot is Prior to installation of this modification it 23.11.2011 BELL 206B Electronic FlightInformation System (EFIS-SV). approved only when configuredwith the 902- must be determined thatthe BELL 206L 00028-01 Control Panel;Activation of Fuel Flow interrelationship between this modification BELL 206L-1 functions requires installation of and any other previouslyinstalled BELL 206L-3 separatelyapproved fuel flow modification and/ or repair will introduce BELL 206L-4 transducers;Installation is not permitted on no adverse effectupon the airworthiness BELL 407 Instrument Flig of the product. 10016223 CHEYENNE TECH EASA.IM.A.S.02471 FAA STC SA01379WI PIPER PA-42-1000 PIPER PA-42-720 Dual Digital Air Data System Installation Qualified for Operation in RVSM Airspace. 10015771 CHIPPEWA AEROSPACE, Inc. EASA.IM.A.S.01810 ST03064AT BAE JETSTREAM 4101 Installation of Honeywell MK VI Enhanced Ground Proximity Warning System (EGPWS) Additional operational limitatiosn may apply for dual operation due to RVSM Altimeter location. 10016183 CHIPPEWA AEROSPACE, Inc. EASA.IM.A.S.02412 FAA STC ST 03080 AT Installation of a Honeywell AAK VI EGPWS. 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 10016184 CHIPPEWA AEROSPACE, Inc. EASA.IM.A.S.02413 FAA STC ST 02898 AT BOMBARDIER CL-600-2B19 Installation of a Honeywell MK V EGPWS. BOMBARDIER CL-600-2C10 (FAA STC ST 02898 AT). 10016185 CHIPPEWA AEROSPACE, Inc. EASA.IM.A.S.02414 FAA STC ST 03336 AT BOMBARDIER CL-600-2B19 Installation of Protective Covers for K4XD Relay. Traffic Alert and Collision Avoidance Systems (TCAS) Processor and Horizontal Stabilizer Control Unit (HSTCU). 10016186 CHIPPEWA AEROSPACE, Inc. EASA.IM.A.S.02415 FAA STC ST 03099 AT BOMBARDIER CL-600-2B19 Installation of a replacement landing gear wiring harness. 10016345 CHIPPEWA AEROSPACE, Inc. EASA.IM.A.S.02662 FAA STC ST2685AT SAAB 340B Installation of FA2100CVF Cockpit Voice SAAB SF340A Recorder in Saab 340 series. 10016437 CHIPPEWA AEROSPACE, Inc. EASA.IM.A.S.02778 FAA STC ST03336AT BOMBARDIER CL-600-2B19 Installs of Protective Covers for the 1K4XD, BOMBARDIER CL-600-2C10 BOMBARDIER CL-600-2D15 BOMBARDIER CL-600-2D24 TCAS and HSTU Processor. 10016506 CHIPPEWA AEROSPACE, Inc. EASA.IM.A.S.02870 FAA STC ST03573AT BOMBARDIER CL-600-2B19 Installs the electrical provisions for Goodrich BOMBARDIER CL-600-2C10 BOMBARDIER CL-600-2D15 BOMBARDIER CL-600-2D24 8730A2 Class 2 Elect. Flt. Bag. 06.09.2007 31.05.2006 03.07.2007 07.04.2008 N/A 29.05.2007 N/A 29.05.2007 N/A 22.02.2008 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.This modific 04/01/2013 Page 154/462 09.04.2008 24.06.2008
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10026871 CHIPPEWA AEROSPACE, Inc. P- FAA STC ST03280AT BAE 125-700 Installation of a Honeywell Flitelink Engine None. 1. Prior to installation of this modification 19.08.2009 EASA.IM.A.S.03213 BAE 125-800 Condition Trend Monitoring- Data Downloader the installer mustdetermine that the BAE 125-800A (ECTM-DD) interrelationship between this modification BAE 125-800B and anyother previously installed HAWKER 750 modification will introduce no adverse HAWKER 800 effectupon the airworthiness of the HAWKER 800 XP HAWKER 850 XP HAWKER 900 XP product.2. The insta 10026882 CHIPPEWA AEROSPACE, Inc. P- FAA STC ST03573AT CL-600-2B19, CL-600-2C10, Installation of a Goodrich Class 2 Electronic Restricted to Configuration 2 as defined in 1) Prior to installation of this modification 19.08.2009 EASA.IM.A.S.03218 CL-600-2D15, CL-600-2D24 Flight Bag Chippewa AerospaceCertification Plan No 601- the installer mustdetermine that the 4620-CP Rev D, dated 24 March 2009. The interrelationship between this modification applicant must submit the final EWIS ICA, if and anyother previously installed applicable, to theAgency by7 June 2010 modification will introduce no adverse effectupon the airworthiness of the product. 2) The inst 10031668 CHIPPEWA AEROSPACE, Inc. REV. 1 FAA STC SA03859AT LIBERTY XL-2 Garmin GTX 330 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. 05.11.2010 10032241 CHIPPEWA AEROSPACE, Inc. FAA STC SA03860AT LIBERTY XL-2 Honeywell KN-62A DME 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. 05.11.2010 10042101 CHIPPEWA AEROSPACE, Inc. FAA STC ST02604AT DHC-8-102,-103,-106 DHC-8-201,-202 DHC-8-301,-311,-314,-315 10042660 CHIPPEWA AEROSPACE, Inc. FAA STC ST02046AT DHC-8-102, DHC-8-103, DHC-8-106, DHC-8-201, DHC-8-202, DHC-8-301, DHC-8-311, DHC-8-314, DHC-8-315. Installation of a Honeywell MK VIII Enhanced Ground Proximity WarningSystem (EGPWS). Installation of a ground service busFAA STC ST02046AT The aircraft must be equipped with the factory installed HoneywellGround Proximity Warning System (GPWS). Prior to installation of this modification it 08.11.2012 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. 12.12.2012 10014984 CHRISTEN-AIRTECH AG EASA.A.S.03276 CESSNA P210N Avionics RetrofitOut: King KMA-24; Sigtronics SPA-400; Dual King KY-196; Dual King KN-53; King KI-525A; trimble TNL-2000; King KT-76A; ARGUS-5000; BF Goodrich WX-1000In: Garmin GMA-347; Dual Garmin GNS-430; Garmin GTX-330; Garmin GMX-200; L-3 WX- 500; Sande Reg: HB-CZK S/N: P21-00860 24.01.2008 10014987 CHRISTEN-AIRTECH AG EASA.A.S.03280 CESSNA P210N Avionics Upgradeby removing:1. GPS-155 1. Reg.: HB-CHJ S/N: P210-0522. Valid for 06.11.2007 GPS2. KX-165 COM/NAV 13. KX-155 this S/N Only.2. Prior to installation of this COM/NAV 24. WX-8 Stormscope5. KMA- modification the installer must determine that 24 Audio Paneland installing:1. GNS-530 the interrelationship between this modification COM/NAV/GPS 12. GNS-430 and any other previously installed modification COM/NAV/GPS 23. WX-500 Stormscope4. will introduce n GMA-347 Audio Panel 10015066 CHRISTEN-AIRTECH AG EASA.A.S.03392 BEECH C90KING AIR GNS 530A, GNS 430A, GAD 42 installation:Removed equipment:- 2 KTR 905 COM 1 & COM 2- 2 KNR 630 NAV 1 & NAV 2- 1 KLN 90B GPS with AK-950 GPS Annunciator- 1 KDM 705A DME with KDI 570 DME IndicatorNew installed equipment:- 1 GNS 530AW COM/NAV/GPS 1 with GAD 4 F-GBLU, SN: LJ-822. 10.09.2008 04/01/2013 Page 155/462
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04/01/2013 Page 1/462 - EASA

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