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 10014920 BAYO S.A.S. EASA.A.S.03167 CESSNA 177RG STC 42/2007 - Modification of radio electric 1. Aircraft must be equipped with HSI 08.02.2008 installation for B-RNAV certification with AP KI525A and S-TEC 60-2 autopilot;2. Prior to coupling. installation of this modification the installer must determine that the interrelationship between this modification and any other previously installed modification will 10015010 BAYO S.A.S. EASA.A.S.03312 CESSNA 182J 54/2006 - IFR BRNAV certification extension of STC Bayo 27/2006 must be already the GNS430 without Autopilot coupling. installed.The Aircraft must be equipped with HSI KI525A. 10015098 BAYO S.A.S. EASA.A.S.03439 REV. 1 FAIRCHILD SWEARINGEN SA 226-T 10015138 BAYO S.A.S. EASA.A.S.03491 FAIRCHILD SWEARINGEN SA 226-T Modification of radio electrical Installation2 VHF The approvam is limited to MSN T-276 F- 21A, 2VOR/ILS/MKR VIR 30A, 2 ATC TDR GLLOGPS use is forbidden for 90, 1 RMI 30 removal2GNS 430 W, 2 MD 41, SID/STAR/ApproachesGPS/Auto Pilot 2 A-30 ACK, 2GTX 330D, 1 KA-33, 1 ST3400 coupling is forbidden below 2000 ft. Installation Modification of radio electrical installation: replacement radar indicator by MFD Garmin GMX200 and/or Concord Batteries. 1. The approval is limited to MSN T-276 F- GLLO;2. Use of GMX 200 limited to radar weather display function;3. Prior to installation of this modification the installer must determine that the interrelationship between this modification and any othe 10015179 BAYO S.A.S. EASA.A.S.03557 PIPER PA-25-235 Modification of radio electrical Limited to S/N 25-74-05726, 25-3109, 25- Prior to installation of this modification the 21.01.2009 installation.Installation of AG-NAV2 GPS 3704, 25-3984, 25-4382, 25-3292,25-2400, 25- installer must determinethat the spreading guidance system not to be used for 4445. interrelationship between this modification navigation, in accordance with "Fiche and any otherpreviously installed d'approbation de conception d'une évolution modification will introduce no adverse No. 53/2007, rev.3 dated 12/12/08". effect uponthe airworthiness of the product. The installati 10015220 BAYO S.A.S. EASA.A.S.03635 BEECH 58 Modification of radio electrical installation for B- The applicability of this STC is limited to the 14.11.2008 RNAV certification with AP coupling Beech 58 S/N TH-488Navigation on SID and STARs prohibited in Terminal AreaUtilisation of GPS prohibited for approachesPrior to installation of this modification the installer must determine that the interrela 10017122 BAYO S.A.S. EASA.R.S.01209 EUROCOPTER FRANCE AS 365N SERI 10032968 BAYO S.A.S. STC 2010-006 HR 100/200, HR100/200 B HR 100/210, HR 100/210 D HR 100/285 TIARA HR100/250 TR, HR 100/285 C 10015726 BAYSYS TECHNOLOGIES, LLC EASA.IM.A.S.01741 FAA STC ST01939LA AIRBUS A319-115 AIRBUS A319-133 BAYO avionics modification no. 16/2005: This STC can be installed only by BAYO installation of- two NAV/COM/GPS GNS 430 technical personal in accordance with BAYO for IFR B-RNAV operations, with their STC definition file n°16/2005-DEF, revision 0, associated MD 41 annunciators, A-30 ACK dated December 19th 2005 or later EASA altitude encoders and KA 33cooling system,- a approved revision Garmin GTX 330 mode S transponder,- two Bendix-King Installation of single EFIS Aspen EFD1000 Pro for VFR navigation. Direct TV - Installation of a tailwind 55 Satellite direct TV receive system Approved software version for ACU and PFD units is 1.1.Navigation coupling to automatic pilot is limited to heading mode. 1. Maximum Tekeoff Weight and Maximum Landing Weight shall be reduced as follows:Takeoff 350 lbs (159 Kg)Landing 410 lbs (186 Kg)2. For airplane(s) modified by this STC, prior to the accumulation of 9,200 total flight cycles from the STC modification, the 10013982 BBJ DESIGN SERVICES LIMITED EASA.A.S.01014 AIRBUS A320-200 Reconfiguration of Passenger Cabin to 180 Economy Class Passengers 10013985 BBJ DESIGN SERVICES LIMITED EASA.A.S.01017 REV. 1 BOEING 737-700 Installation of 44 Passenger Seats, seats BOEING 737-800 power supply and in seat power supply system on Boeing-BBJ128 Reynard J2000 double seats,safety equipment, carpet and new wardrobes. Installation of General Dynamics In Seat Power System. 10013986 BBJ DESIGN SERVICES LIMITED EASA.A.S.01018 Floor Structure rework. 1. This STC is restricted to Boeing 767-3Z9 Registration G-VKNG, Serial Number 23765.2. 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 airc 24.01.2008 05.03.2008 08.04.2008 19.01.2006 Prior to installation of this modification it 10.12.2010 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.Install 04/01/2013 Page 110/462 23.11.2006 17.01.2005 24.10.2005 08.06.2005
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10013987 BBJ DESIGN SERVICES LIMITED EASA.A.S.01019 Replacement of a Lufthansa Technik IFE 1. This STC is approved only for the product 17.03.2005 System with an ITAN IFE 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. 10014047 BBJ DESIGN SERVICES LIMITED EASA.A.S.01129 BOEING 757-200 Enhanced Mode S Surveillance System completion and activation 01.04.2005 10014048 BBJ DESIGN SERVICES LIMITED EASA.A.S.01130 BOEING 767-300 Enhanced Mode S Surveillance System completion and activation 01.04.2005 10014232 BBJ DESIGN SERVICES LIMITED EASA.A.S.01395 AIRBUS A321 Installation of Koito 24B/C and 148Y seats for Dragonair 11.11.2005 10014321 BBJ DESIGN SERVICES LIMITED EASA.A.S.01573 AIRBUS A330 Installation of In Seat Power Supply Korean Air Airbus A330 25.01.2006 10014388 BBJ DESIGN SERVICES LIMITED EASA.A.S.01674 Replacement of Aft G4B Galley. 27.06.2006 10014520 BBJ DESIGN SERVICES LIMITED EASA.A.S.02601 REV. 1 BOEING 767-300ER Installation of a MAS2000E in Flight Entertainment System on Austrian Airlines B767-300ER aircraft -- 02.02.2007 10014567 BBJ DESIGN SERVICES LIMITED EASA.A.S.02668 BD-700-1A11 Installation of an Electronic Flight Bag (EFB) on This approval of thie installation does not 03.11.2006 A/C S/N 9089Modification Summary List: include any approval of the suitability, integrity, BBJ745 issue 1CCL: BBJCCL205 issue or accuracy of the EFB hardware, software, 1ADoC: Mod. Sum. Sh. & Certificate of Design data base, display, controls or lighting.The iss. 25/10/2006 capability of the system to "perform its intended function" has not been 10014658 BBJ DESIGN SERVICES LIMITED EASA.A.S.02815 BOEING 747-400 Interior changes required on Cathay Pacific Boeing 747-400 aircraft MSN 27132 for BE Aerospace Flight Structures. 10.05.2007 10014665 BBJ DESIGN SERVICES LIMITED EASA.A.S.02822 REV. 1 BOEING 757-200 SERIES Cabin Reconfiguration on Boeing 757-230 aircraft -- 02.03.2007 10014770 BBJ DESIGN SERVICES LIMITED EASA.A.S.02962 BOEING 747-400 Interior Changes required on Cathay Pacific Prior to installation of this modification the 02.07.2007 Boeing 747-400 for BE Aerospace Flight installer must determine that the Structures. interrelationship between this modification and any other previously installed modification will introduce no adverse effect upon the airworthiness of the product. The install 10014774 BBJ DESIGN SERVICES LIMITED EASA.A.S.02966 BOEING 767-300 Installation of an in-seat power supply system and reconfiguration of business class seating. 10014784 BBJ DESIGN SERVICES LIMITED EASA.A.S.02984 BOEING 757-200 Installation of fixed Emergency Locator Transmitter 10014250 BEECHCRAFT BERLIN AVIATION GmbH EASA.A.S.01472 REV. 2 B200 Installation of Cloud Research and Seeding System This EASA STC 10014250, REV. 2 reflects the transfer of STCEASA.A.S.01472 Revision 1 from Scandinavian Avionics Design GmbH toBeechcraft Berlin Aviation GmbH 10042830 BEECHCRAFT BERLIN AVIATION GmbH C90GTI Laser Scanner and Weather Research Application. 10017062 BELL HELICOPTER TEXTRON CANADA, EASA.IM.R.S.01497 TCCA STC NO. SH05-2 BELL 212 Ltd BELL 412 BELL 412 EP 10016755 BELL HELICOPTER TEXTRON, Inc. EASA.IM.R.S.01084 SR09397RC BELL 206A BELL 206B TCCA SH05-2 “Cold Weather Use of Kerosene Fuels”. This STC is approved only for the product configuration as defined in the approved design data referred to in the paragraphs "Description" and “Associated Technical Documentation”. Compatibility with other aircraft/engine configurations shall be determined 30.05.2007 N/A 13.04.2007 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 27.09.2010 For mission equipment installed under the wingSpeeds are limited to vNO = 150 KIAS, and vNE = 169 KIASFlights into areas with known icing conditions is not permitted. For The installation of this modification by third persons is subject towritten permission of the approval holder and disposal of the approvedappropriate further limitation see AFMS, Doc. No. D18-B11- documentation. Prior to installation of this 01, Section II modification it must be determined thatthe interrelationship 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 STC ST09397RCIncrease in takeoff weight Aircraft effectivity is as follows: • This STC is from 1.451 Kg (3200 lbs) to 1.520 Kg (3350 lbs limited to 206A or 206B aircraft that are when modified in accordance with Bell Model qualified for and configured with the 65 inch 206 Series Service Instructions BHT-206-SI- diameter tail rotor. • 206A S/N 4 thru 660, 129 dated July 12, 2004, or later FAA and 672 thru 715 if modified to a Model 206B approved revision. by incorporation of Ser 04/01/2013 Page 111/462 19.12.2012 24.11.2008 01.02.2006
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04/01/2013 Page 1/462 - EASA

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