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 10035215 PRECISE FLIGHT, Inc. FAA STC SA2622NM FALCON 50 Installation of Precise Flight Pulse Light Control This approval is restricted to the following Prior to installation of this modification it 06.06.2011 system in Falcon 50aircraft.EASA validation of Pulselite units:2400-25-4-4 / 2400-25-4-4-1 / must be determined thatthe FAA STC SA2622NM for Falcon 50 aircraft. 2400-25-4-4-2 / 2401S / 2401.This approval interrelationship between this modification does not cover the physical installation of the and any other previouslyinstalled system.Physical installation of the system in the modification and/ or repair will introduce aircraft should be dulys no adverse effectupon the airworthiness of the product. 10015539 PRECISION CONVERSIONS LLC EASA.IM.A.S.01423 ST1529SE BOEING 757-200 SERIES Conversion from Passenger to Freighter Configuration (including Main Deck Cargo Door, Crew Entry Door, Interior & Associated Systems. 27.10.2006 10014487 PREMIAIR AIRCRAFT ENGINEERING EASA.A.S.02549 BEECH 390 Satellite Telephone Installation 11.05.2006 10017110 PREMIAIR AIRCRAFT ENGINEERING EASA.R.S.01087 AS 365N2 Premiair Aircraft Engineering Modification 05- 010.KLN 900 GPS Receiver Installation. 10017111 PREMIAIR AIRCRAFT ENGINEERING EASA.R.S.01088 AS 365N2 Premiair Aircraft Engineering Modifications 05- 007 & 05-009. Modifications embodied, since manufacture, in Brazil & South Africa. Also modifications embodied to meet EASA & JAR OPS-3 requirements. 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. 1. Aircraft Serial No. 6393 Only2. 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 10017121 PREMIAIR AIRCRAFT ENGINEERING EASA.R.S.01208 AS 355N IFR Upgrade with EFIS 40 Installation 1. 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. 10017155 PREMIAIR AIRCRAFT ENGINEERING EASA.R.S.01261 REV. 2 AS365N2, AS365N3, SA365N1 Installation of Honeywell MK XXI EGPWSNote: This revision is to amend an existing EASA STC (RefP-EASA.R.S.01261 rev. 1) to add the AS 365N3 model None This STC is approved only for the product configuration as defined inthe approved design data referred to in the paragraphs "Description" and"Associated Technical Documentation" Prior to installation of this modification it must be determined thatthe inter 10017160 PREMIAIR AIRCRAFT ENGINEERING EASA.R.S.01268 AS 355 F1 Install a Honeywell KLN90B GPS -- 07.07.2006 10017174 PREMIAIR AIRCRAFT ENGINEERING EASA.R.S.01289 REV. 2 AS365N2, AS365N3, SA365N1 Installation of Honeywell KTA 870 Traffic None This STC is approved only for the product 01.02.2010 Advisory SystemNote: This revision is to configuration as defined inthe approved amend an existing EASA STC (RefP- design data referred to in the paragraphs EASA.R.S.01289 rev. 1) to add the AS365N3 "Description" and"Associated Technical model Documentation" Prior to installation of this modification it must be determined thatthe inter 10017175 PREMIAIR AIRCRAFT ENGINEERING EASA.R.S.01290 REV. 2 AS365N2, AS365N3, SA365N1 Installation of Honeywell KMD 850 Multi Function DisplayNote: This revision is to amend an existing EASA STC (RefP- EASA.R.S.01290 rev. 1) to add the AS 365N3 model 10.08.2005 11.08.2005 16.11.2005 01.02.2010 None This STC is approved only for the product 01.02.2010 configuration as defined inthe approved design data referred to in the paragraphs "Description" and"Associated Technical Documentation" Prior to installation of this modification it must be determined thatthe inter 10017227 PREMIAIR AIRCRAFT ENGINEERING EASA.R.S.01397 S-76B Traffic Advisory System Installation. 26.05.2008 10017233 PREMIAIR AIRCRAFT ENGINEERING EASA.R.S.01411 AS 355 N Installation of a Honeywell KMD850 Prior to installation of this modification the 05.11.2007 Multifunction Display replacing the existing installer must determine that the IN812A Radar Indicator plus GC360 Radar interrelationship between this modification and Graphics Computer and Interfacing with an any other previously installed modification will existing Honeywell RDR2000. introduce no adverse effect upon the airworthiness of the product. The install 10027205 PREMIAIR AIRCRAFT ENGINEERING P-EASA.A.S.03982 BEECH 390 (PREMIER 1) Cabin configuration change None Prior to installation of this modification the 14.09.2009 installer must determinethat the interrelationship between this modification and any otherpreviously installed modification will introduce no adverse effect uponthe airworthiness of the product. 04/01/2013 Page 362/462
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10039783 PREMIAIR AIRCRAFT ENGINEERING A-60+ Installation of Cabin Safety Equipment 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. 23.05.2012 10015562 PREMIER AIR CENTER, Inc. EASA.IM.A.S.01460 ST01884CH FAN JET FALCON SERIES D FAN JET FALCON SERIES E FAN JET FALCON SERIES F MYSTERE FALCON 20-C5 MYSTERE FALCON 20-D5 MYSTERE FALCON 20-E5 MYSTERE FALCON 20-F5 MYSTERE FALCON 200 10027600 PREMIER AIRCRAFT, LLC P- EASA.IM.A.S.02677 10029073 PROTOPLANE SPECIAL MISSION AIRCRAFT 10034751 PROTOPLANE SPECIAL MISSION AIRCRAFT 10038293 PROTOPLANE SPECIAL MISSION AIRCRAFT 10038491 PROTOPLANE SPECIAL MISSION AIRCRAFT 10039039 PROTOPLANE SPECIAL MISSION AIRCRAFT 10039373 PROTOPLANE SPECIAL MISSION AIRCRAFT FAA STC ST01951LA MF50 BASIC CONFIGURATION EASA Validation of FAA STC ST01951LA:Installation of TFE731-4-1C engine part number 3075900-1, per HoneywellService Bulletin TFE731-72-3703, dated January 19, 2007 on the MF50basic aircraft configuration in accordance with Flight Test Associates,Inc. Maste Installation of a Honeywell Mark VIII Enhanced 1. EASA approved Flight Manual Supplement, Ground Proximity Warning System with Terrain Premier Air Center Document 11-327B001, Display Revision I/R, or later EASA approved revision isa required part of this STC (Configuration- 01)2. EASA approved Flight Manual Supplement, Premier Air Center Document 11- 327B0 Not Applicable Flight Manual Supplement FTA-PA- 001019, Revision IR dated 22nd January2007 was found to contain incorrect data and has been replaced withFlight Manual Supplement FTA-PA- 001019, Revision C dated 30th September2009. All Revision IR Flight Manuals have been r EASA.A.S.03952 BEECH 200 Video transmission mast under a Beech 200. All associated Audio/Video Relay electronic systems and antennas must beturned off during VOR navigation and before beginning the approach. AS 350 B, -D, -B1, -B2 AS 350 BA, -BB, -B3 BN-2 BEZU installation on a BN-2 rev2 du 27/01/2012. AS355E, AS355F, AS355F1 AS355F2, AS355N, AS355NP 29.06.2006 13.10.2009 Prior to installation of this modification it 01.03.2010 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. Installation of video transmission equipment. 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 28.04.2011 Video transmission equipment When antenna holder PP-10-A601 is installed VNE is limited to 120 kts;When rack PP-10- A421 is installed, carriage of passengers in front seatsis prohibited;When racks PP-10- 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. 03.02.2012 Prior to installation of this modification it 21.02.2012 must be determined thatthe interrelationship between this modification and any other previouslyinstalled A401c or PP-A461 are installed, a maximum of modification and/ or repair will introduce 2passengers in rear seats is permitted no adverse effectupon the airworthiness of the product. The ap EC135 T1, T2, T2+, P1, P2, P2+ Installation of a Max-Viz EVS 1500 vision Limited to EC135 equipped with CPDS and enhancement system.Installation of EVS 1500 FCDS. system for Protoplane change project PP-015 asdefined in PP-015-MDL-01. Prior to installation of this modification it 02.04.2012 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. MF50 Attachment provisions on Falcon 50 S/N 011. Limited to S/N 011. 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. 30.04.2012 04/01/2013 Page 363/462
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04/01/2013 Page 1/462 - EASA

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