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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 10035668 SKY IMD Inc. REV. 1 SEE APPROVED MODEL LIST Installation of Sensor Pod and wiring for This STC is for installation of the sensor pod The installation of this modification by 08.07.2011 passenger operated monitoringsystem and wiring from thesensor pod into fuselage. third persons is subject towritten This STC does not include power to the permission of the approval holder and sensorpod or the sensor control unit.Limitations disposal of the approvedappropriate as defined in the applicable Aircraft Flight documentation. Prior to installation of this ManualSupplements. modification it must be determined thatthe interrelationship 10015785 SKY INTERNATIONAL Inc. EASA.IM.A.S.01841 REV 1 SA10463SC AVIAT HUSKY A-1B Installation of a Lycoming model IO-360-A1D6 The engine must be de-rated to 196 HP (see 23.08.2006 engine (derated to 196 HP) and MT Propeller Installation Instructions for details).The Airplane model MTV-15-B/205-58 propeller in Flight Manual Supplement No 55009-18, accordance with Installation Instructions No Revision IR or later EASA approved revision, 1101, Revision C dated 8 May 2006, or later must be used with this modification.The approved revision approved Noise Level is 81.6 dB(A). 10035483 SKYE AVIONICS Ltd. TCCA STC SH11-14 BELL 407 Installation of "Check Engine Instruments" Audio Alert System. 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 27.06.2011 10042298 SKYTECH, INC. EASA.IM.A.S.00604 FAA STC ST01851NY PA46-310P 1- Skytech Inc. Airplane Flight Manual Supplement, HTW-494-782-100 FAAApproved December 31, 2003, is required for this modification.2- This STC is approved only for the product configuration as defined inthe approved design data referred to in the paragrap 02.03.2005 10016790 SKYTRAC SYSTEMS Ltd. EASA.IM.R.S.01137 REV. 2 TCCA STC SH05-42 BELL 407 SkyTrac ISAT-100 Airborne Position/Data 1. Equipment configuration: ISAT-100 (no 13.02.2006 EUROCOPTER DEUTSCHLAND Communicator System Installation.TCCA STC mod.)/mod A, or later TCCA approved major BO-105 SH05-42 Issue no 1 dated 12 September 2005 mod.2. This STC references specified interfacing equipment that is approved via this data. The ISAT-100 equipempment is capable of being interfaced to additional aircr 10016798 SKYTRAC SYSTEMS Ltd. EASA.IM.R.S.01151 REV. 2 TCCA STC SH03-30 ISSUE 4 BELL 212 BELL 412 BELL 412 CF BELL 412 EP EUROCOPTER FRANCE SA 365C EUROCOPTER FRANCE SA 365C1 EUROCOPTER FRANCE SA 365N SIKORSKY S-61N SIKORSKY S-76A SIKORSKY S-76C 10016927 SKYTRAC SYSTEMS Ltd. EASA.IM.R.S.01313 TCAA STC SH03-30 ISSUE 5 EUROCOPTER FRANCE AS 365C EUROCOPTER FRANCE AS 365C1 EUROCOPTER FRANCE AS 365N EUROCOPTER FRANCE EC 155B Installation of SkyTrac ISAT-100 Airborne 1. This STC references specific interfacing Position/Data Communicator SystemRevison 1 equipment that is approved via this data. to add: BK-117 A-1, A-3, A-4, B-1 and B-2 The ISAT-100 equipment is capable of being modelsRevision 2 to add: Eurocopter SA 365 interfaced to additional aircraft systems for C, C1, N, EC 155B wich approval is beyond the scope of this STC. Such interfaces may Installation of SkyTrac ISAT-100 Airborne This STC references specific interfacing Position/ Data Communication System Note: equipment that is approved via this data. The This application is to amend an existing EASA ISAT 100 equipment is capable of being STC (Ref P-EASA.IM.R.S.001151 Rev. 1) to interfaced to additional aircraft systems for add the SA 365 C,C1,N, EC 155B helicopter which approval is beyond the scope of this models STC. Such interfaces may need further ap 10030917 SKYTRAC SYSTEMS Ltd. TCCA STC SA09-93 SkyTrac Flight Following / SATCOM Installation in acc. with TCCA STCSA09-93:ISAT-100 transceiver installed in aft zone of aircraft, Dual elementGPS/Iridium antenna installed on upper fuselage, optional DVI-250 andCDP-250 control panels installed at centre 21.03.2007 21.03.2007 None None 12.07.2010 10030918 SKYTRAC SYSTEMS Ltd. TCCA STC SA09-80 CESSNA 208, 208B SkyTrac Flight Following / SATCOM Installation None in acc. with TCCA STCSA09-80, Issue 1:ISAT- 100 transceiver installed in aft zone of aircraft, Dual elementGPS/Iridium antenna installed on upper fuselage, optional DVI-250 andCDP-250 control panels installed a None 12.07.2010 04/01/2013 Page 408/462
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10031247 SKYTRAC SYSTEMS Ltd. REV. 2 TCCA STC SH10-24 ISSUE 2 206A, 206A-1, 206B, 206B-1, SkyTrac ISAT Airborne Position/Data STC EASA.IM.R.S.01137 is a prerequisite to Prior to installation of this modification it 22.12.2010 206L, 206L-1, 206L-3, 206L-4, Communicator this installation. must be determined thatthe 407 interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product. 10031804 SKYTRAC SYSTEMS Ltd. TCCA STC SA06-85 200/200C/200T/200CT/A200/A200 SkyTrac ISAT Position Data Communicator C 300/300LW/B300/B300C/1900D A200CT/B200/B200C/B200T/B200 CT System Installation. 10033276 SKYTRAC SYSTEMS Ltd. TCCA STC SH10-24 ISSUE 2 EC 120 B Sky Track ISAT AIRBORNE POSITION / COMMUNICATION UPGRADEThe modification upgrades an existing ISAT-100 Airborne Position / DataCommunicator system installation to an ISAT-200 system(This EASA approval validates the TCCA STC SH10-24, 10033865 SKYTRAC SYSTEMS Ltd. TCCA STC NO. SH10-24 EC 135 P1(CDS),EC 135 P1(CPDS) EC 135 P2(CPDS),EC 135 P2+ EC 135 T1(CDS),EC 135 T1(CPDS) EC 135 T2(CPDS),EC 135 T2+ 10036485 SKYTRAC SYSTEMS Ltd. TCCA STC SH10-24 AS 355 E, AS 355 F, AS 355 F1 AS 355 F2, AS 355 N Issue 2) Sky Track ISAT AIRBORNE POSITION / COMMUNICATION UPGRADEThe modification upgrades an existing ISAT-100 Airborne Position / DataCommunicator system installation to an ISAT-200 system(This EASA approval validates the TCCA STC SH10-24, Issue 2) Sky Track ISAT AIRBORNE POSITION / COMMUNICATION UPGRADEThe modification upgrades an existing ISAT-100 Airborne Position / DataCommunicator system installation to an ISAT-200 system(This EASA approval validates the TCCA STC SH10-24, Issue 3 on thetype/mode 10036492 SKYTRAC SYSTEMS Ltd. TCCA STC SH10-24 AS 350 B, AS 350 B1, AS 350 B2 Sky Track ISAT AIRBORNE POSITION / AS 350 B3, AS 350 BA, AS 350 D COMMUNICATION UPGRADEThe modification upgrades an existing ISAT-100 Airborne Position / DataCommunicator system installation to an ISAT-200 system(This EASA approval validates the TCCA STC SH10-24, Issue 3 on thetype/mode 10041706 SKYTRAC SYSTEMS Ltd. TCCA STC SH10-51 AW139 Installation of a SkyTrac ISAT-100/ISAT-200 Position Data Communicator(Canadian STC SH10-51 issue 2) 10014444 SLINGSBY ADVANCED COMPOSITES LTD. EASA.A.S.02495 REV. 1 BEECH 76 Introduction of Bendix/King KCS 55A Compass, KX165 NAV/COM, KR87 ADF, King KN62A DME & KI229 Systems 10013975 SMA - SOCIETE DE MOTORISATIONS EASA.A.S.00774 REV. 7 1. 182M, 182N, 182P, 182Q,182R 2. F182-P, F182-Q 10016495 SMA ENGINES INC. EASA.IM.A.S.02857 FAA STC SA03302AT CESSNA 182Q CESSNA 182R -DET C-09-503 Air Supply circuit modification- DET C-08-508 Introduction of new powerplant limitations-DET C-07-521 Kelly Aerospace alternator ES7024-16 Installation-DET C-08- 510 Modification of the intercooler inlet and outlet nozzlesgeometry.-DJC-STC-C182 Installation of Societe de Motorisations Aeronautiques (SMA) Aircraft Diesel Engine (ADE) model SR305-230-1 (or SR305-230 convertedto model SR305-230-1 by incorperation of SMA Service Bulletin SB-01- 76-002), MT propeller model MTV-9-BS/198- 58B peopeller an 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. 15.09.2010 None EASA.IM.R.S.01137 is a pre-requisite to this approval.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 adver none EASA.IM.R.S.01137 is a pre-requisite to this approval.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 adver None This STC references specified interfacing equipment that is approved viathis data. The ISAT -200 is capable of being interfaced to additionalaircraft systems for which approval is beyond the scope of this STC.Such interfaces may need further approval.EASA. 11.01.2011 15.02.2011 12.09.2011 None This STC references specified interfacing 13.09.2011 equipment that is approved viathis data. The ISAT -200 is capable of being interfaced to additionalaircraft systems for which approval is beyond the scope of this STC.Such interfaces may need further approval. EASA 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. 09.10.2012 Applicable to Cessna 182R, Q, P, N, M and Reims Aviation F182Q and Pmodified in accordance with STC SMA EASA.A.S.00774 and later approvedrevisions. 20.06.2006 Prior to installation of this modification it 04.05.2011 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. None. 06.11.2008 04/01/2013 Page 409/462
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04/01/2013 Page 1/462 - EASA

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