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 10038678 AEROCONSEIL B777-200 0527-01: eXPhone System Installation on B777-Per AFM Supplement 0527-01-A-2301.This Prior to installation of this modification it 07.03.2012 200 aircraft. modification is limited to Boeing 777-200 must be determined thatthe MSN29953, exceptsimilarity demonstrated per interrelationship between this modification Document 0001-01-B-0914 (Classification and any other previouslyinstalled ofModification Change Procedure for GSM modification and/ or repair will introduce connectivity System). no adverse effectupon the airworthiness of the product. 10038812 AEROCONSEIL REV. 1 A330-301 / -302 / -303 A330-321 / -322 / -323 A330-341/ - 342 / -343 10038876 AEROCONSEIL B777-200 0542-01: WiFi internet access system installation on B777-200 10039705 AEROCONSEIL A330-201 / -202 / -203 A330-223 / -243 10040592 AEROCONSEIL A330-201 / -202 / -203 A330-223 / -243 Panasonic eXPhone System activation on none The following modifications are 21.08.2012 A330-300 with eXconnectThis STC installs a prerequisites to the installation ofthis STC Panasonic eXphone System allowing, in :- Delta Engineering STC ref : ODA-2224conjunctionwith other devices, the use of 01 - EASA Approval 10037166 Rev 1or cellphones during flight.This revision 01 extends later revisions of the above listed the STC applicability to a second aircraftco documents approved by EASAPrior to installation of this modificatio Panasonic eXPhone System activation on A330 with eXConnect and Rack P/NRD- AA903023This STC installs a Panasonic eXphone System allowing, in conjunctionwith other devices, the use of cellphones during flight. Panasonic eXPhone System Activation on A330 with eX2 IFE and eXconnect.This STC installs a Panasonic eXphone System allowing, in conjunctionwith other devices, the use of cellphones during flight. 10041655 AEROCONSEIL 777-200LR & 777-300ER 0465-01: eXPhone System Activation on B777- 200LR/300ER 10042771 AEROCONSEIL A320-111,-211,-212,-214,-215 A320-216,-231,-232,-233 10038123 AEROCONTROLEX GROUP, INC. FAA STC ST02798CH 1. B767-200/-300/-400ER 2. B777-200/-300/-300ER/-200LR - per AFMS 0542-01-A-2301- Airworthiness Prior to installation of this modification it 21.03.2012 Limitations per ICA Document 0542-01-A-2211 must be determined thatthe aremandatory- This modification is limited to interrelationship between this modification Boeing 777-200 MSN29953, exceptsimilarity and any other previouslyinstalled demonstrated per Document 0001-01-B-0914 modification and/ or repair will introduce (Classification ofModification Change Proc no adverse effectupon the airworthiness of the product. None. The following modification is prerequisite 18.05.2012 to the installation of thisSTC : -,,Delta Engineering STC "installation of Panasonic GCS" - EASA Approval10038944 Prior to installation of this modification it must be determined thatthe interrelationship between None. The following modifications are prerequisites to the installation ofthis STC : -,,Airbus Minor Change ref : 48818 - Approved under Airbus DOAEASA.21J.031, on 03 December 2002-,,Delta Engineering STC ref : ODA- 2269-01 - EASA Approval 10038944or later revisi per AFMS 0465-01-A-2301 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. 12.07.2012 04.10.2012 Installation of SICMA Dragonfly seats for Indigo none Prior to installation of this modification it 18.12.2012 on A320 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. Installation of an AeroControlex Potable Water Level Sensor Assembly P/N8430-000000 10013930 AERODATA AG EASA.A.S.00277 REV. 2 B300 Installation of Aerodata Automatic Flight Inspection System AD-AFIS-112. 10013931 AERODATA AG EASA.A.S.00278 REV. 2 BEECH 300 Flight Data Recorder (FDR) integration into Hawker Beechcraft King Air B300 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. 20.01.2012 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. 06.05.2011 04/01/2013 Page 18/462 19.10.2007
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10013988 AERODATA AG EASA.A.S.01020 BEECH B200 Installation of TCAS 2000 with RCZ 852 Mode 1. This STC is approved only for the product 11.02.2005 BEECH B200T S Transponders 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. 10013989 AERODATA AG EASA.A.S.01021 BEECH B200 Installation of UNS 1-F Flight Management 11.02.2005 BEECH B200T BEECH B300 System 10013991 AERODATA AG EASA.A.S.01023 DORNIER D328-100 DORNIER D328-300 AeroPhone IRIDIUM SATCOM Installation 14.09.2005 10013993 AERODATA AG EASA.A.S.01024 REV. 9 DORNIER 328-100 Installation of Maritime Surveillance System on None Prior to installation of this modification the 30.01.2012 Dornier 328-100including SAR Radar, FLIR, installer must determinethat the and optional IR/UV Scanner Revision 4: interrelationship between this modification Functional/optional upgrade to the radar and any otherpreviously installed system and mission software tooptimize search modification will introduce no adverse and rescue operation. Hardware upgrade t effect uponthe airworthiness of the product. The installati 10014244 AERODATA AG EASA.A.S.01454 BEECH B200 SUPER KING AIR Installation of Aerodata Flight Inspection System AD-FIS-9 25.01.2006 10014515 AERODATA AG EASA.A.S.02591 Installation of Aerodata Flight Inspection System AD-AFIS-0220. 31.10.2006 10014516 AERODATA AG EASA.A.S.02592 LBA STC SA 1320 BEECH B200 Installation of Normarc Flight Inspection System NM3625B.NOTE: this STC supersedes existing LBA STC SA 1320 None 07.09.2006 10014785 AERODATA AG EASA.A.S.02985 BEECH B300 Installation of EGPWS Mark VI Upgrade in Compatibility of this modification with other 16.04.2007 B300. previously approved modifications must be determined by the installer. 10014930 AERODATA AG EASA.A.S.03184 REV. 1 KING AIR 300 Installation of an Aerodata Flight Inspection Airplane must be equipped with Collins ProLine 26.10.2007 System AD-AFIS-230 II to be eligible for this STC. 10015136 AERODATA AG EASA.A.S.03489 REV. 3 B200, B200C, B200GT Installation of Aerodata Flight Inspection For AD-AFIS-120, Mod. No. B200-11.01:Only The installation of this modification by 08.06.2011 System- AD-AFIS-120, Mod. No. B200-11.01, applicable for aircraft model B200 and third persons is subject towritten or- AD-AFIS-250, Mod. No. B200-12.01, or- B200GT, and when equippedwith Collins permission of the approval holder and AD-AFIS-250, Mod. No. B200-12.02, or- AD- Proline 21, and preconditions as defined disposal of the approvedappropriate AFIS-250, Mod. No. B200-14.01 in DesignDescription, Installation of Aerodata documentation. Prior to installation of this 10015166 AERODATA AG EASA.A.S.03536 REV. 1 CESSNA 550 CITATION II Additional Cockpit Information DisplayThe FIS, Doc. No. DES-A/C-836, Rev. 2,dated 27- modification it must be determined thatthe interrelationship Prior to installation of this modification the 26.01.2009 current STC EASA.A.S.03536 covers the installer must determine that the installation of an Aerodata Flight Inspection interrelationship between this modification and System (FIS). To further reduce the required any other previously installed modification verbal communication and therefore the will introduce no adverse effect upon the workload of the cockpit crew and the FIS opera airworthiness of the product. 10015182 AERODATA AG EASA.A.S.03561 PILATUS PC-12 Modification as surveillance aircraft 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. 10015235 AERODATA AG EASA.A.S.03660 LEARJET 31A Installation of Aerodata Flight Inspection System (FIS) 10015270 AERODATA AG EASA.A.S.03745 BEECH 300 Installation of an Aerodata Flight Inspection System AD-AFIS-111 10017098 AERODATA AG EASA.R.S.01022 REV. 1 EUROCOPTER DEUTSCHLAND BK117 B EUROCOPTER DEUTSCHLAND BK117 C - Cockpit Arrangement for ADAC BK 117 Fleet for IFR operation- Re-arrangement of Cockpit Instruments for a harmonized Cockpit Layout of several BK 117 Helicopters. Furthermore integration of a dual Garmin GNS430 equipment and GTX330 Mode S Transponde 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. 1. Airplane must be equipped as stated in Chapter 1.3.1 of EASA approved Aerodata Certification Program, Doc. No. CP-B300- 13.01,Revision 0, dated 12-Jan-2009, or later approved revision2. Prior to installation of this modification the installer must 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 pro 04/01/2013 Page 19/462 11.11.2008 16.10.2008 13.03.2009 10.02.2009
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04/01/2013 Page 1/462 - EASA

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