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 10017240 BUCHER LEICHTBAU AG EASA.R.S.01428 FOCA STC 25-20-62 EUROCOPTER DEUTSCHLAND 1. Installation of ambulance and rescue 22.11.2007 EC-135- equipment.2. Extension of Validity of former FOCA STC Z - 25-2062 to the new model versions T2+/P2+ of EC 135. 10017275 BUCHER LEICHTBAU AG EASA.R.S.01509 FOCA STC 25-20-64 EC-135-P1, EC-135-P2, Installation of VIP-EC135-AC63 Bucher VIP Not applicable The approval holder shall fulfil the 14.11.2008 EC-135-P2+, EC-135-T1 Equipment(Revision of FOCA STC FOCA Z 25- obligations of Part 21, EC-135-T2, EC-135-T2+ 20-64 Issue 3) Paragraph21.A109. Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repai 10027691 BUCHER LEICHTBAU AG FOCA 25-20-102 REV. 4 SEE AIRCRAFT ALLOCATION 16G New Generation Stretcher P/N 1120030 S/N: as per Aircraft Allocation Table E043-01- This STC revision replaces EASA STC 21.08.2012 REV 3 TABLE SeriesMinor change to EASA STC 10027691- 12 Rev. E of 31/07/2012This installation 10027691 Rev. 3Prior to installation of E043-01-12 REV. E OF 31/07/12 Stretcher integration P/N 1120030-Series on constitutes an approval for installation only this modification it must be determined Airbus A321-211 foraircraft serial numbers as stated in the thatthe interrelationship between this Master Document List. For anyadditional modification and any other configurations as per Aircraft Allocati previouslyinstalled modification and/ or repair will introduce no adverse 10027884 BUCHER LEICHTBAU AG P-EASA.A.S.03796 REV. 2 SEE EASA APPROVED AML P/N 1120030-300 - 16g New Generation This STC does not constitute an approval for Prior to installation of this modification it 01.07.2010 Stretcher XLRevision of the EASA STC installation. Compliancewith following must be determined thatthe 10027884 to include A380 a/c type in requirements below need to be demonstrated interrelationship between this modification theapplicability through adesign approval for Stretcher and any other previouslyinstalled installation in aircraft per approvedModel list: § modification and/or repair will introduce 25.561(d) § 25.785(a) § 25.785(h) § 25. no adverse effectupon the airworthiness of the product. 10029211 BUCHER LEICHTBAU AG REV. 5 EC135 ARA-EC135-AC67 BUCHER Ambulance and Rescue System (ARA):Rev. 5 to EASA STC 10029211: - Installation of a hot compartment 10030689 BUCHER LEICHTBAU AG P-EASA.A.S.03797 SEE EASA APPROVED MODEL LIST intocenter cabinet Record of revisions: Rev 4: - editorial change to EASA approval certificate (correction by EASA)Rev 3: (Minor Chang 16g New Generation Stretcher P/N 1120020- 300 - (NGS) 10030758 BUCHER LEICHTBAU AG P-EASA.A.S.03712 ERJ-170() E006-14-08 - P/N 1120050 9G NGS XL Stretcher: Installation of aremovable 9g New Generation Stretcher (NGS) 10030810 BUCHER LEICHTBAU AG FOCA Z25-20-57 REV. 1 EC135 P1(CDS), EC135 P1(CPDS) EC135 P2(CPDS), EC135 P2+ EC135 T1, EC135 T2, EC135 T2+ 10031757 BUCHER LEICHTBAU AG P-EASA.A.S.03984 REV. 6 SEE AIRCRAFT ALLOCATION TABLE E-043-02-12 REV. A DATED 10/12/2012 10038839 BUCHER LEICHTBAU AG EASA.A.S.03919 REV. 1 SEE EASA APPROVED MODEL LIST Installation of ARA-EC135-AC60 Ambulance and Rescue SystemNew revision covers:STC issuance under EASA format at revision 0, Exchange of Suction Unitwith new P/N 1355185,adding P2+ and T2+ at the list of EC135 models. This STC revokes the STC 10030489 ATS 16g Stretcher P/N: 1123000-000 / -100 / - 200 / -300 / -390 / -400 /-500 / -590Major Change to STC 10031757 Rev. 4-Installation envelope expansion for Boeing B787- Reduction of installation limitations-Introduction of the Aircraft Allocation Table Small person restraint system P/N 1120040 for use on 16G New GenerationStretcher P/N 1120020-XXX. Compliance with NVIS compatible flight decks Prior to installation of this modification it 21.05.2012 must be demonstrated by theinstaller when must be determined thatthe ARA-EC135-AC67 with NVIS compatible cabin interrelationship between this modification lighting shallbe installed into NVIS equipped and any other previouslyinstalled rotorcraft. modification and/ or repair will introduce no adverse effectupon the airworthiness of the product. This STC does not constitute an approval for Prior to installation of this modification it 01.07.2010 installation. Compliancewith following must be determined thatthe requirements below need to be demonstrated interrelationship between this modification through adesign approval for Stretcher and any other previouslyinstalled installation in aircraft per approvedModel list: § modification and/ or repair will introduce 25.561(d) § 25.785(a) § 25.785(h) § 25. no adverse effectupon the airworthiness of the product. -Limitations iaw. User Manual E017-01-08- TGM 25/12 addressed per CRI D-1 A.S.3712 None. 13.07.2009 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. 29.11.2011 This STC constitutes an approval for installation only for aircraftserial numbers as stated in the Master Document List. For any additionalconfiguration as per Aircraft Allocation Table, the requirements asstated in the Master Document List have to be demo Small person restraint to be used only on stretcher P/N 1120020-XXX.Occupant limitations as per General Arrangement drawing 1120040 and UserManual E017-04- 08. This EASA STC amends STC 10031757 Rev. 5Prior 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 14.12.2012 effectupon The installation of this modification by 20.03.2012 third persons is subject towritten permission of the approval holder and holding and disposal ofthe approved appropriate documentation.Prior to installation of this modification it must be determined thatthe interre 04/01/2013 Page 146/462
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10041271 BUCHER LEICHTBAU AG FOCA STC 25.20.42 SEE APPROVED MODEL LIST ATL Airtransport Litter System P/N 123000 - 1. This STC does not constitute an approval for This EASA STC replaces STC-FOCA 25- 03.09.2012 (ISSUE 5) Seriesincluding customers options:P/N 123000- installation. Compliancewith following 20-42 This Supplemental Type Certificate 000 (Demo ATL)P/N 123000-110 requirements below need to be demonstrated is approved only for the (Lufthansa)P/N 123000-241 (AUA-2)P/N by a designapproval for Stretcher installation in productconfiguration as defined in the 123000-27 (Emirates-2) aircraft per applicable approvedmodel list: JAR approved design data referred to 25.561(d) JAR 25.785(a), JAR inparagraph "Description". The approval holder shall fulfill the obligations of Par 10014019 BUSINESS & COMMUTER AIRCRAFT EASA.A.S.01073 CESSNA 550 CITATION II Installation of TCAS II system in accordance with MDL BCA 70-00 rev. 3 dated 18/03/05 10014024 BUSINESS & COMMUTER AIRCRAFT EASA.A.S.01079 BEECH 1900D Emergency Transmitter Kannad 406 MHz installation on Beechcraft 1900 D. 10014049 BUSINESS & COMMUTER AIRCRAFT EASA.A.S.01131 REV. 1 BEECH 300 BEECH B300 Installation of KLN 900 GPS with EFIS-85 according to STCEASA.A.S.01131. This STC is applicable to s/n 550-0622 04.04.2005 1. This STC is limited to Beechcraft 1900 s/n UE-1 and up.2. Required Pre-Modification: any existing EASA approved ELT doubler Airplane Flight Manual Supplement No. BCA/61 must be used with this modification. 10014088 BUSINESS & COMMUTER AIRCRAFT EASA.A.S.01182 BEECH C90 Installation of Weather Radar RDR-2000 Modification limited to Beech C90 S/N LJ-684 BEECH C90 A and Becch C90A S/N LJ-1526 10014121 BUSINESS & COMMUTER AIRCRAFT EASA.A.S.01231 BEECH C90 A Skywatch SKY497 TCAS I installation on 1. AFMS No 68/BCA rev 0 of April 2005 must Beech C90A be used when modification is installed2. Modification is limited to Beech C90A S/N LJ- 1526 10014190 BUSINESS & COMMUTER AIRCRAFT EASA.A.S.01332 REV. 1 CESSNA 500, CITATION Dual GARMIN GPS installation: GNS-430A + 1. S/N 550-0324 and 500-03612. This STC CESSNA 550 CITATION II GNS-530A in accordance with MDL BCA 74- is approved only for the product configuration 00 rev 6 dated 19/07/05 as defined in the approved design data referred to in the paragraph "Description". Compatibility with other aircraft/engine configurations shall be determined by t 20.01.2005 BEECH 300 /B300 - F-GPRH - SN FA 226. The approval holder shall fulfil the obligations of Part 21,Paragraph21.A109.Prior to installation of this modification it must be determined thatthe interrelationship between this and any other previously installedand/ or repair will introduce no adverse 06.02.2012 10014220 BUSINESS & COMMUTER AIRCRAFT EASA.A.S.01381 BEECH 1900D Installation of ACSS TCAS 2000 System. 08.07.2005 10014335 BUSINESS & COMMUTER AIRCRAFT EASA.A.S.01590 BEECH 1900C, AIRLINER Installation of ACSS TACS 2000 System on This STC is limited to Beech 1900 C SN UC- 11.10.2005 Beech 1900C. 115 10014387 BUSINESS & COMMUTER AIRCRAFT EASA.A.S.01673 BEECH 1900D Installation of a TCAS II System This STC is applicable to Beechcraft 1900 model D, all Serial Numbers 05.12.2005 10014616 BUSINESS & COMMUTER AIRCRAFT EASA.A.S.02745 BEECH 1900D Installation of VIP configuration in aft ward This modification limits 14 passengers 09.11.2006 cabin and passive noise reduction kit maximum. 10014831 BUSINESS & COMMUTER AIRCRAFT EASA.A.S.03046 BEECH C90 Installation of dual Mode S transponder system 22.05.2007 BEECH E90 BEECH F90 (GARMIN GTX-330 or GTX-330D). 10014835 BUSINESS & COMMUTER AIRCRAFT EASA.A.S.03051 EASA STC 2004-2474 CESSNA 500 Major Modification: change of a pilot HSI 1. See original STC : DGAC-F nr. F-CIM81- 02.03.2007 against EHSI ; re-wiring of existing equipment SF-000102. This STC is approved only for power supply to the emergency bus.Note: This the product configuration as defined in the EASA STC supersedes EASA STC 2004- approved design data referred to in the 2474. paragraphs "Description" and “Associated Technical Documentation”. Compatibility wi 10015029 BUSINESS & COMMUTER AIRCRAFT EASA.A.S.03338 BEECH 1900C, AIRLINER Installation of a toilet cargo aera. Modification limited to Beech 1900C s/n UC- 168. 10015038 BUSINESS & COMMUTER AIRCRAFT EASA.A.S.03351 BEECH 1900 28-230 volts inverter installation on Beech 1900 Airplane flight manual supplement BCA 102, series according to modification file BCA102, rev. 0, dated 30-10-2007 or later approved rev. 0, dated 30-10-2007 or later approved revisions must be used when modiifcation is revisions. applied. 10015058 BUSINESS & COMMUTER AIRCRAFT EASA.A.S.03380 BEECH 1900C, AIRLINER Installation of a galley in the FWD right area of 1. Must be installed on Beech 1900C (S/N the A/C. UC-1 and after);2. 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 10015059 BUSINESS & COMMUTER AIRCRAFT EASA.A.S.03381 REV. 1 BEECH 1900C, AIRLINER Installation of a galley in the FWD right area of the A/C. Must be installed on Beech 1900C (S/N UC-1 and after). 04/01/2013 Page 147/462 17.03.2005 30.05.2005 31.01.2007 10.01.2008 19.11.2007 29.01.2008 29.01.2008
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04/01/2013 Page 1/462 - EASA

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