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 10016725 EUROCOPTER CANADA Ltd. EASA.IM.R.S.01023 REV. 1 TCCA STC SH 96-32 AS350BA, AS350B2, AS350B3 Left-side pilot configuration Note: Revision of None Prior to installation of this modification it 13.12.2010 EASA STC ref. EASA.IM.R.S.01023 being a must be determined thatthe validation ofTCCA STC SH 96-32 at issue 7. interrelationship between this modification This STC revision is validation of TCCASTC and any other previouslyinstalled SH 96-32 at issue 11 and includes the left-side modification and/ or repair will introduce pilot configurationchange made to no adverse effectupon the airworthiness of the product. 10016728 EUROCOPTER CANADA Ltd. EASA.IM.R.S.01031 TCCA STC SH 97-15 AS 350 B/BA/B1/B2/B3/D Installation of LH and/or RH Cargo pods 1. This STC is approved only for the product (Squirrel Cheeks")Master Drawing List MDL-94- configuration as defined in the approved design 004 and associated maintenance data referred to in the paragraph "Description". instructionsFlight manual supplement FMS- Compatibility with other aircraft/engine ECL-9, revision 2 or later TCCA approved configurations shall be determined by the revisions installer. 10016747 EUROCOPTER CANADA Ltd. EASA.IM.R.S.01073 TCCA STC SH 96-31 AS 350 B/BA/BB/D/B1/B2/B3 AS 355 E/F/F1/F2 EUROCOPTER FRANCE AS 355F2 Relocation of higher capacity battery to tail boomMaster Drawing List MDL-04-003 and MDL-96-001 associated installation procedure and maintenance instructions.Flight Manual Supplement attached to STC SH96-31 issue 6, approved 25 March 1996 or later TCCA ap 10016825 EUROCOPTER CANADA Ltd. EASA.IM.R.S.01195 TCCA STC SH00-1 ISSUE 3 AS 350 B, AS 350 B1, AS 350 B2 Installation of high visibility main and aft cabin AS 350 B3, AS 350 BA, AS 350 D doorsrefer to TCCA STC SH00-1 issue N°3, July 25, 2003 10016845 EUROCOPTER CANADA Ltd. EASA.IM.R.S.01221 TCCA STC SH05-18 AS 350 B/B1/B2/B3/BA/D/D1 Installation of Forward Short High-visibility Doors (350-202414). 10016935 EUROCOPTER CANADA Ltd. EASA.IM.R.S.01321 TCCA STC SH97-34 ISSUE 3 AS 350 B/B1/B2/B3/BA/D AS 355 E/F/F1/F2/N Installation of Forward Opening Rear Cargo Doors.(Modification approved by TCCA under STC SH97-34 Issue 3). 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. Refer to TCCA STC SH00-1 issue N°3, July 25, 2003 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 1; This STC is approved only for the production 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.Installation of th 10017000 EUROCOPTER CANADA Ltd. EASA.IM.R.S.01410 TCCA STC SH03-33 EC 130 B4 Cargo Pods Installation 12.06.2008 10038250 EUROCOPTER CANADA Ltd. TCCA STC SH94-29 1- AS350B, BA, B1, B2, B3, D Title: Left-Hand Litter KitDescription: Installation Configuration must be in accordance with Prior to installation of this modification it 31.01.2012 2- AS355E, F, F1, F2, N, NP of Left-Hand Litter Kit P/N 350-200034 or Eurocopter Canada MasterDrawing List No. must be determined thatthe P/N350-200194 in accordance with Eurocopter MDL-99-001, Issue F, or later approved interrelationship between this modification Canada Master Drawing List No.MDL-99-001. revisions.Approved configurations are listed in and any other previouslyinstalled The Left-Hand Litter Kit provides med-evac the attached table. modification and/ or repair will introduce capabilities fornon-EMS dedicate no adverse effectupon the airworthiness of the product. 10041637 EUROCOPTER CANADA Ltd. TCCA STC SH12-10 EC130B4 Door handle installation (P/N 120-200014)This STC is the validation of TCCA STC SH12-10 (issue date -February 10,2012) 10041736 EUROCOPTER CANADA Ltd. TCCA STC SH11-35 EC130B4 Glare Shield Modification P/N 130-885114This STC is the validation of TCCA STC SH11-35 (issue No. 1 dtdSeptember 20, 2011) 10033870 EUROCOPTER DEUTSCHLAND GmbH P-EASA.R.S.01568 EC120B Installation on an EC120B helicopter of a ETSO-certified (ETSO C113)Moving Map system (MT VisionAir EPIII) 12.10.2005 12.10.2005 12.05.2006 05.07.2007 18.10.2007 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. 03.10.2012 None The approval holder shall fulfill the obligations of Part 21, Paragraph21.A.118A. Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or re 11.10.2012 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. 15.02.2011 04/01/2013 Page 210/462
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10039633 EUROCOPTER DEUTSCHLAND GmbH LBA STC EMZ NR. 0654/3058 BO105 LS A-3 Title: Superlifter Conversion Kit 105- None The implementation of the modified 24.05.2012 8003331Description:Original STC: The model cargo hook 105-803101 is onlyapproved BO105 LS A-3 is changed in accordance after conversion of the helicopter in withdrawing No. 105-800331. The changed accordance with drawingNo. 105model is called "Superlifter".Revision 1: The 800331.This STC is valid in conjunction Airworthiness Limitations related to EMZ Nr. with the EASA TCDS R.011 in 0654/3 theapplicable version. This Supplemental Type 10041899 EUROCOPTER DEUTSCHLAND GmbH EC 120 B Installation of GTN 650 Unit on EC 120B 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. 23.10.2012 10017128 EUROCOPTER UK Ltd. EASA.R.S.01216 EUROCOPTER FRANCE AS 355N 10017136 EUROCOPTER UK Ltd. EASA.R.S.01230 REV. 1 EC135-P1+, EC135-P2+ Change to existing EASA STC EC135-T1, EC135-T2, EC135-T2+ EASA.R.S.01230 - NVG Compatible LightingSystem - to extend the approved Night Vision Goggle types to allowsingle pilot operations and to include the latest EC135 types. Integration of minor and major changes to 1. Limited to AS355N, S/N 5708 OE-XDM2. Storm Light, 406MHz ELT, STBY Altimeter, This STC is approved only for the product Exhaust heat shield, Autopilot, ADI, COM/NAV, configuration as defined in the approved design Transponder, Audiopanel, GNS 530, Compass data referred to in the paragraph "Description". System and Instrument Panel Compatibility with other aircraft/engine configurations shall be determined b 13.10.2005 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. The fi 20.11.2009 10017177 EUROCOPTER UK Ltd. EASA.R.S.01295 EUROCOPTER DEUTSCHLAND Variable External Playload Configuration MBB-BK Refer to above RFM Supplements 16.03.2007 10017199 EUROCOPTER UK Ltd. EASA.R.S.01348 EUROCOPTER DEUTSCHLAND Installation of Honeywell Avionics MKXXII As defined in the AFM Supplement No. 34 03.04.2007 EC-135- EGPWS 10017219 EUROCOPTER UK Ltd. EASA.R.S.01376 EUROCOPTER FRANCE AS Re-Instatement of approval for Category A 13.04.2007 365N3 Operations reference FAR 29 Amendment 16 10017253 EUROCOPTER UK Ltd. EASA.R.S.01456 EUROCOPTER FRANCE AS Installation of NAT 611-014 Voice Warning 365N3 Generator (AVAD). 10017256 EUROCOPTER UK Ltd. EASA.R.S.01463 REV. 1 EUROCOPTER DEUTSCHLAND Installation of FreeFlight 2101 I/O Approach Prior to installation of this modification the EC-135- Plus GPS with navigation information installer must determine that the interfaced to the aircraft FCDS and the aircraft interrelationship between this modification and AFCS for coupled autopilot operations, iaw any other previously installed modification will Drawing No. A3/1351114-100. introduce no adverse effect upon the airworthiness of the product. The install 10017260 EUROCOPTER UK Ltd. EASA.R.S.01469 EUROCOPTER DEUTSCHLAND EC-135 10017264 EUROCOPTER UK Ltd. EASA.R.S.01475 EUROCOPTER DEUTSCHLAND EC-135- 10017269 EUROCOPTER UK Ltd. EASA.R.S.01489 EUROCOPTER FRANCE AS 355NP 10017270 EUROCOPTER UK Ltd. EASA.R.S.01490 EUROCOPTER FRANCE AS 355NP Installation of honeywell EGPWS Mk XXII. Installation of Honeywell EGPWS XXII iaw drwg. no. A3/1351134-100 with aural and display based on ECUK modification MHL/135/1134. Installation of STAR SAFIRE HD FLIR (based on EC UK modification MHL/135/1116).. ECUK modifcation MCH/A/135/1075 must be installed as prerequisite. 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. The i Installation of a Leo II FLIR System 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. Installation of SFIM 85T31 3 Axis Autopilot 0 Prior to installation of this modification the System 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 211/462 22.04.2008 11.12.2008 01.09.2008 14.11.2008 13.01.2009 14.01.2009
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04/01/2013 Page 1/462 - EASA

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