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 10016792 FUGRO AIRBORNE SURVEYS EASA.IM.R.S.01140 TCCA STC SH 98-37 EUROCOPTER FRANCE AS 350 Installation of Fugro Airborne Surveys Electro- 1. STC SH 98-37 Supplemental Flight Manual 11.10.2005 B Magnetometer Boom & Geosurvey Equipment 4537-01 Revision 01 approved 18 July 2000 EUROCOPTER FRANCE AS 350 installation or later approved revisions.2. DECA Aviation B1 Flight Manual Supplement No. 453707 EUROCOPTER FRANCE AS 350 Revision 1, dated 18 July 2000 or later B2 approved revision3. This STC is approved only EUROCOPTER FRANCE AS 350 B3 EUROCOPTER FRANCE AS 350 BA EUROCOPTER FRANCE AS 350 D EUROCOPTER FRANCE AS 355E EUROCOPTER FRANCE AS 355F EUROCOPTER FRANCE AS 355F1 EUROCOPTER FRANCE AS 355F2 for 10016428 G&D AERO PRODUCTS INC. EASA.IM.A.S.02767 FAA STC SA7063NM BEECH 200 BEECH 300 Installation of Acrylic window liners None 05.03.2008 10014342 GAMA ENGINEERING Ltd. EASA.A.S.01602 BEECH 200 Major Avionic Upgrade 06.04.2006 10014355 GAMA ENGINEERING Ltd. EASA.A.S.01620 BEECH 200, SUPER KING AIR Major Avionic System Upgrade 19.12.2005 10014357 GAMA ENGINEERING Ltd. EASA.A.S.01622 REV. 1 BEECH B200C, SUPER KING AIR Ground Use Battery 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. 10.03.2011 10014389 GAMA ENGINEERING Ltd. EASA.A.S.01675 REV. 1 BAE.125 SERIES 800 Title: Upgrade of the dual Flight Management System (FMS).Description of change: The original dual Honeywell FMZ-900 FMS isupgraded to a dual Honeywell FMZ-2000 FMS. The installer must determine whether this design change is compatiblewith previously approved modifications. Prior to installation of this modification it 05.10.2012 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. 10014502 GAMA ENGINEERING Ltd. EASA.A.S.02570 BEECH 200 Mode S Transponder Installation. Beech 200 Series. As per AFMS706001 Issue 1 06.02.2008 10014542 GAMA ENGINEERING Ltd. EASA.A.S.02629 REV. 1 A340-311, A340-312, A340-313. Child Restraint System - CRS - Installation in Limitations in accordance with § 4 - Limitations Prior to installation of this modification it 10.12.2012 A340-300 of the above mentionedDDP, ref. No. DDP- must be determined thatthe 1785-026.All cabin interiors must be evaluated interrelationship between this modification for compatibility of the ChildRestraint System and any other previouslyinstalled (CRS). The CRS is not approved for modification and/ or repair will introduce aeroplanes that arenot defined by § 4 no adverse effectupon the airworthiness of the product. 10014543 GAMA ENGINEERING Ltd. EASA.A.S.02630 REV. 1 A340-643 Child Restraint System - CRS - Installation in A340-600 Limitations in accordance with § 4 - Limitations Prior to installation of this modification it 10.12.2012 of the above mentionedDDP, ref. No. DDP- must be determined thatthe 1785-026.All cabin interiors must be evaluated interrelationship between this modification for compatibility of the ChildRestraint System and any other previouslyinstalled (CRS). The CRS is not approved for modification and/ or repair will introduce aeroplanes that arenot defined by § 4 no adverse effectupon the airworthiness of the product. 10014544 GAMA ENGINEERING Ltd. EASA.A.S.02631 REV. 1 B747-400 Installation of MAGE Child Restraint System as 1. This STC only covers the installation of the Prior to installation of this modification it 20.06.2012 detailed in ModificationLeaflet for Modification MAGE Child RestraintSystem on Virgin Atlantic must be determined thatthe no. B744-1795. Airways Boeing 747-400 Aircraft, as defined interrelationship between this modification inMAGE DDP1785-026 and in accordance with and any other previouslyinstalled the instructions and limitationsdefined in MAGE modification and/ or repair will introduce Crew Manual Supplement TN 17 no adverse effectupon the airworthiness of the product. 10014626 GAMA ENGINEERING Ltd. EASA.A.S.02764 HAWKER 800 XP Installation of a L-3 Avionics F1000 Flight Data Recorder. This Installation is intended for compliance with JAR-OPS 1.715. This STC however grants no operational approval to this installation, that will need to be obtained from the State of registry for the particular aircraft involved as defined in JAR OPS 1.715 04/01/2013 Page 226/462 17.10.2006
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10014627 GAMA ENGINEERING Ltd. EASA.A.S.02765 BEECH 200 Enhanced Mode S Upgrade. Beech 200/300 SeriesAFM Supplements AFMS730001 and AFMS730002. 12.03.2008 10014768 GAMA ENGINEERING Ltd. EASA.A.S.02960 CESSNA 425 Installation of Traffic Advisory System As defined in the AFM supplement 08.03.2007 10014769 GAMA ENGINEERING Ltd. EASA.A.S.02961 CESSNA 425 Installation of Garmin GNS 530 & GTX330 As per AFM Supplements. 08.03.2007 10015050 GAMA ENGINEERING Ltd. EASA.A.S.03369 CESSNA 500, CITATION Upgrade of Mode S Transponder for Enhanced Surveillance 05.03.2008 10015153 GAMA ENGINEERING Ltd. EASA.A.S.03516 HAWKER HS 125-700 SERIES Dual FMS Upgrade. 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.2. 14.08.2008 10015186 GAMA ENGINEERING Ltd. EASA.A.S.03570 CESSNA 525 Upgrade of Mode S transponders for enhanced surveillance. 13.06.2008 10015247 GAMA ENGINEERING Ltd. EASA.A.S.03684 HAWKER 700 Introduction of a Sandel ST3400 Class A Prior to installation of this modification the 15.12.2008 terrain awareness warning system. 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. 10017226 GAMA ENGINEERING Ltd. EASA.R.S.01395 REV. 1 BO 105 S (CBS-4) The Pyrotechnic Display System:Carriage and none Prior to installation of this modification it 24.02.2011 deployment of static flares and roman candle must be determined thatthe typepyrotechnics, installed each side on interrelationship between this modification external dispenser mounts attachedto landing and any other previouslyinstalled gear skids and interfaced with cabin control box modification and/ or repair will introduce to sequenceignition. Note: this no adverse effectupon the airworthiness of the product.The app 10017247 GAMA ENGINEERING Ltd. EASA.R.S.01445 BELL 412 Installation of a dual electronic horizontal situation indicator (EHSI) system. 1. The EHSI system must have a minimum software level of Eight (8) installed in the symbol generators.2. The YELLOW symbol generator “SG” flag or display unit “DU” flag must not be visible prior to departure.3. Autopilot coupled ADF tracking is no 10027113 GAMA ENGINEERING Ltd. P-EASA.A.S.03842 PA-28 Aspen EFD1000 System None None 07.09.2009 10027314 GAMA ENGINEERING Ltd. PIPER PA32 ALL SERIES Installation of Aspen EFD1000 PFD Prior to installation of this modification the 21.09.2009 installer must determinethat the interrelationship between this modification and any otherpreviously installed modification will introduce no adverse effect uponthe airworthiness of the product.The installatio 10027637 GAMA ENGINEERING Ltd. EASA.A.S.03763 REV. 2 F28 MARK 0070 Interior Refurbishment and System Upgrade None. None. 26.11.2012 10027657 GAMA ENGINEERING Ltd. REV. 1 PA-23-235, PA-23-250 Installation of Garmin G500/G600 EFIS None Prior to installation of this modification it 21.10.2010 PA-E23-25 PFD/ND 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. 10027818 GAMA ENGINEERING Ltd. REV. 2 PA32 ALL SERIES Installation of Garmin G500/G600 PFD/ND This change is limited to the configuration defined in Change StatementCS1100-02 Issue 2 or later approved revision. None 01.04.2010 10028029 GAMA ENGINEERING Ltd. PA-34-200, PA-34-200T, Installation of Aspen EFD1000 PFD as add on Only applicable for airplanes/preconditions as The installation of this modification by 26.11.2009 PA-34-220T defined Section 1.1,"Installation planning" of third persons is subject towritten Doc. No. CS1106-01, "Change Statement", permission of the approval holder and Issue2, or later approved issue For approved holding and disposal ofthe approved Software Level of Aspen EFD1000 refer to appropriate documentation. Prior to "Limitations,Conditions, Exemptions" installation of this modification it must be determined thatthe interr 10028069 GAMA ENGINEERING Ltd. 182 SERIES Installation of Aspen EFD1000 PFD None None 30.11.2009 10029002 GAMA ENGINEERING Ltd. PA-31 Installation of defence aid antennas and None Applicable to Piper PA 31 s/n 31-815 25.02.2010 systems only. 10029092 GAMA ENGINEERING Ltd. PA-31 ATC transponder upgrade for Mode S enhanced surveillance Not Applicable Not Applicable 03.03.2010 04/01/2013 Page 227/462 22.05.2008
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04/01/2013 Page 1/462 - EASA

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