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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 10015850 STAR AVIATION Inc. EASA.IM.A.S.01950 ST02989AT CESSNA 500 The modification will consist of a composite 12.05.2006 CESSNA 501 structure with a metal faceplate wich will be CESSNA 550 fitted over the center of the existing CESSNA 551 Glareshield. An area of the existing glareshield CESSNA S550 will be removed to allow for wires to be routed to the annunciators and switc 10036456 STAR AVIATION Inc. P- EASA.IM.A.S.00285 REV. 1 FAA STC ST02861AT B747-400 Installation of Connexion by Boeing Next Generation Antenna and SateliteData System in accordance with Star Aviation Inc. Master Data ListR44-0163, Revision CP, Dated May 12, 2011 or later approved revision 10041648 STAR AVIATION Inc. EASA.IM.A.S.00286 REV. 1 FAA STC ST02942AT 747-400 Installation of Cabin Wireless Local Area Network (CWLAN) in accordancewith Star Aviation Inc. Master Data List R44-0175, Revision G, datedOctober 13, 2004, or later FAA approved revisions and Provisionalinstallation of a Panasonic Avionics Corporation eXP 10016830 STARFLEX L.L.C. EASA.IM.R.S.01201 FAA STC SH7962SW-D EUROCOPTER FRANCE AS 355F2 Installation of two Allison 250-C20R engines and enhanced anti-torque system in accordance with AHC drawing list 355A82- 1755 Revision D dated November 5, 1990 or later FAA approved revision 10016832 STARFLEX L.L.C. EASA.IM.R.S.01203 SH7961SW-D Installation of two Allison 250-C20R engines in accordance with AHC drawing list 355A82- 1753 Revision H dated November 5, 1990 or later FAA approved revision 10035635 STARFLEX L.L.C. AS 355 F1, AS 355 F2 Compliance of C20R installation with BCAR 10035081 STC ACQUISITION, LLC FAA STC ST01567LA G-1159 (GULFSTREAM II) G-1159A (GULFSTREAM III) G-1159B (GULFSTREAM IIB) Section G and confirmation ofability of C20R to fly one engine inoperative profiles. Installation of a pylon mounted ejector system with new design thrustreversers, to show compliance with ICAO Annex 16, Volume 1, Amendment 9,Chapter 3 noise requirements. None Aircraft Flight Manual Supplement R44- 0300 Rev. IR dated October 16,2004 is a required part of this STC.Instruction for Continued Airworthiness Star Aviation Document No #R44-0273, Rev. D, dated June 20, 2011 must be made available to theoperator at the ti None AFM Supplement R44-0293, Revision A, dated October 18, 2004 shall be onboard the modified aircraftInstructions for Continued Airworthiness Document # R44-0182 Rev. IRdate June 16, 2004, Document # R44-290, Rev. IR dated July 15, 2004 andDocument # R44-0427 1. The present STC is the validation of the FAA STC SH7962SW-D, last amended on 01 February 2006.2. Compatibility of this modification with previously approved modifications of the aircraft must be determined by the installer. 1. The present STC is the validation of the FAA STC SH7961SW-D, last amended on 01 February 2006.2. Compatibility of this modification with previously approved modifications of the aircraft must be determined by the installer. none When fitted with STC EASA.IM.R.S.01203, the AS355F1 is certificated asGroup A under BCAR Section G ("Equivalent to Category A" in accordancewith JAR OPS 3, ACJ OPS 3.480 (a)(1)&(a)(2)) when the followingconditions are met (as listed in Model G-1159, (Gulfstream II)1),,Aircraft without Aircraft Service Change (ASC) 81, “62,500 PoundIncreased Gross Weight Modifications, or those with a Maximum (ramp)weight less than 62,500 lb are not eligible for this modification.2),,Aircraft with ASC 200 09.09.2011 23.10.2012 16.01.2007 16.01.2007 06.07.2011 the TCDS EASA.R.146) Prior to installation of this modification it 24.05.2011 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. 10014128 STC TWENTY ONE LIMITED EASA.A.S.01238 REV 1 DC-9-80 (MD-80) SERIES Introduction of FlightVu Cabin Surveillance System 21.06.2006 10014129 STC TWENTY ONE LIMITED EASA.A.S.01239 BOEING 757-200 Introduction of SSR Mode S Enhanced Surveillance 30.05.2005 10014131 STC TWENTY ONE LIMITED EASA.A.S.01241 BAE ATP Rework to Landing Gear Emergency Up-Lock Release Mechanism 15.11.2005 10014185 STC TWENTY ONE LIMITED EASA.A.S.01323 REV 1 FOKKER F.27 MARK 500 FOKKER F.27 MARK 600 Use of TRA-45A Display Indicator 30.01.2006 10014209 STC TWENTY ONE LIMITED EASA.A.S.01361 REV 1 BAE ATP Introduction of Class E Compartment for LFD Modified Aircraft. 1. Flight Manual Supplement S21.FMS-0008; 09.04.2008 10014210 STC TWENTY ONE LIMITED EASA.A.S.01362 REV 1 BAE ATP Introduction of Freight Loading & Restraint This major change is limited to embodied into a 09.04.2008 System for LFD Modified Aircraft. Bae aircraft previously modified for the installation of a large cargo door at the rear of the fuselage in accordance with Bae Service Bulletin ATP-52-036 and with the installation of a main cabin Class 'E' c 10014211 STC TWENTY ONE LIMITED EASA.A.S.01363 BAE ATP Installation of AAR Freight Loading System This STC may only be embodied into BAe ATP aircraft previously modified for the installation of a large cargo door at the rear of the fuselage, in accordance with British Aerospace Service Bulletin SBATP-52-036 (Modification M60138A), with a barrier net in 30.01.2006 04/01/2013 Page 420/462
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10014252 STC TWENTY ONE LIMITED EASA.A.S.01477 BOEING 757-200 Introduction of Honeywell MKV Enhanced Ground Proximity Warning System (EGPWS) 22.09.2005 10014253 STC TWENTY ONE LIMITED EASA.A.S.01478 BOEING 757-200 Introduction of Honeywell GNSSU Receiver 22.09.2005 10014344 STC TWENTY ONE LIMITED EASA.A.S.01606 LOCKHEED L1011 - TRISTAR Introduction of a stand-alone GPS receiver 22.03.2006 10014392 STC TWENTY ONE LIMITED EASA.A.S.01681 SAAB SF340A Saab 340 Class E Cargo CompartmentThis -- 12.02.2007 SAAB SF340B significant major change, designed by STC WP- EASA.A.S.01681Twenty One Limited, will convert the main passenger cabin to a class E cargo compartment for the carriage of freight 10014417 STC TWENTY ONE LIMITED EASA.A.S.01738 SAAB 340 SAAB 340B Saab 340 Bulk Cargo Restraint System (as defined in document S21 MDL-0034). This major change will introduce transverse nets at discrete positions in the aircraft main cabin (converted to Class E under STC Twenty One Limited major change S21.25-63-1015) to 10014418 STC TWENTY ONE LIMITED EASA.A.S.01739 SHORTS SD3-60 Introduction of ACAS II & Single Mode S Transponders with Elementary Surveillance. 10014443 STC TWENTY ONE LIMITED EASA.A.S.02494 BAE ATP Introduction of Rockwell Collins ACAS II and Dual Mode S Transponder System 10014446 STC TWENTY ONE LIMITED EASA.A.S.02499 CESSNA 550 CITATION II Introduction of an AirCell Satellite Telephone System ST 3100 to the aircraft.This modification installs the handset into an arm rest on the rear starboard side of the aircraft. The Satellite Phone Transceiveris installed in the mid cabin drinks stowage on 10014447 STC TWENTY ONE LIMITED EASA.A.S.02500 BOEING 767-200-300 Introduction of SSR Mode S Enhanced Surveillance System. 10014477 STC TWENTY ONE LIMITED EASA.A.S.02539 BAE 146 Introduction of T2 CAS Collision Avoidance & Terrain Awareness System 10014522 STC TWENTY ONE LIMITED EASA.A.S.02605 AIRBUS A310 SERIES Installation of Honeywell MK V EGPWS.This supplemental Type Certificate installs a Terrain Awareness Warning System. This STC must be used in conjunction with EASA STC EASA.A.S.01681 "Saab 340 Class E Cargo Compartment". 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. 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. This design change should be embodied concurrently with or after the embodiment of STC Twenty One Limited minor design change S21.23-29-1000. 23.04.2007 13.03.2006 16.02.2006 09.06.2006 Boeing 767-200/300 series.It is a condition of 12.10.2007 this STC that transponders of different manufacturers must not be intermixed, refer to STC 21 IPC supplement S21.TEC-0033 for further details. - 22.05.2006 10014523 STC TWENTY ONE LIMITED EASA.A.S.02606 BOEING 727 SERIES Introduction of Emergency Locator Transmitter 15.06.2006 10014564 STC TWENTY ONE LIMITED EASA.A.S.02664 BOMBARDIER CL-600-2B16 (604) Introduction of Passenger Cabin Interior 22.06.2006 10014597 STC TWENTY ONE LIMITED EASA.A.S.02717 BAE ATP Rework of LH Passenger Door 11.05.2007 10014628 STC TWENTY ONE LIMITED EASA.A.S.02766 BAE 146/AVRO 146 SERIES Introduction of T2CAS Collsion Avoidance & Terrain Awareness Warning System -- 03.11.2006 10014667 STC TWENTY ONE LIMITED EASA.A.S.02824 BOEING 757-200 SERIES Reduction of Over-Wing Emergency Exits from This STC is approved only for the product 22.12.2006 4 to 2. 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. 10014683 STC TWENTY ONE LIMITED EASA.A.S.02846 SD3-60 Introduction of Honeywell MK VI EGPWS 07.12.2006 10014711 STC TWENTY ONE LIMITED EASA.A.S.02883 BAE 146 Introduction of Hoenywell RDR-4B Weather Radar System 10.07.2007 10014723 STC TWENTY ONE LIMITED EASA.A.S.02900 FOKKER F.27 MARK 050 Introduction of Rockwell Collins Dual ADF-60 Instructions for Continued Airworthiness: STC 20.06.2007 FOKKER F.27 MARK 0502 System in the F27 Mark 200. This installation Tewnty One Limited Change Supplement FOKKER F.27 MARK 0604 replaces the existing Bendix Dual ADF Manual document S21.TEC-0094 Revision 0, FOKKER F.27 MARK 100 System.In accordance with STC Twenty One dated 21/03/2002, or later EASA approved FOKKER F.27 MARK 200 Limited Master Drawing List document S21. revision. FOKKER F.27 MARK 300 MDL-0264 dated 14/12/2006 or later EASA FOKKER F.27 MARK 400 FOKKER F.27 MARK 500 FOKKER F.27 MARK 600 FOKKER F.27 MARK 700 appr 04/01/2013 Page 421/462 28.11.2007
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04/01/2013 Page 1/462 - EASA

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