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 10015794 MASS SYSTEMS, EASA.IM.A.S.01853 FAA STC ST00961LA 1.AEROSPATIALE ATR 42-200 Installation of MASS Systems Fire Extinguisher 08.04.2008 2.BELL 204B Cartridge as replacement for Walter Kidde 3.BOEING DC-8-71 Aerospace fire extinguisher cartridges in fire 4.BOEING DC-9-14 extinguisher bottles installed in the airplane 5.CESSNA 401 models noted on the EASA approved model 6.CESSNA 500 7.EMBRAER EMB-120 8.SAAB SF340A 9.SIKORSKY S-76A AEROSPATIALE ATR 42-300 AEROSPATIALE ATR 42-320 AEROSPATIALE ATR 42-500 AEROSPATIALE ATR 72-101 AEROSPATIALE ATR 72-102 AEROSPATIALE ATR 72-201 AEROSPATIALE ATR 72-202 AEROSPATIALE ATR 72-211 AEROSPATIALE ATR 72-212 AEROSPATIALE ATR 72-212A BELL 205A BELL 205A-1 BELL 205B BELL 212 BELL 412 BELL 412 CF BELL 412 EP BOEING DC-8-61 BOEING DC-8-61F BOEING DC-8-63 BOEING DC-8-63F BOEING DC-8-71F BOEING DC-8-72 list dtd 02 April 2008 (which exc 10015795 MASS SYSTEMS, EASA.IM.A.S.01854 FAA STC ST00885LA BOEING 1. AIRBUS DC-8-73 A300 SEE LIST Installation of Mass Systems, Inc. fire This STC is approved only for the product 24.01.2007 10. BOEING 737 SERIES extinguisher cartridges as replacements for configuration as defined in the approved design 11. BOEING DC-9 SERIES SEE Pacific Scientific fire extinguisher cartridgesin data referred to in the paragraphs "Description" LIS fire extinguisher bottles installed in the airplane and “Associated Technical Documentation”. 12. BOEING MD11 SEE LIST models noted on the EASA Approved Model Compatibility with other aircraft/engine 13. BOEING 747SP SEE LIST 14. BOEING 757 SEE LIST 15. BOEING 767 SEE LIST 16. BOMBARDIER CL-600 SEE LIST 17. EMBRAER MB120 MB145 18. JETSTREAM 4101 18. SAAB 340A 340B 2.A319 A310 SEE LIST 3. A330 SEE LIST 4. A340 SEE LIST 5. BOEING 747 SEE LIST 6. FOKKER F.27 MARK 100 SEE LI 7. F.47 MARK 1000 SEE LIST 8. RAYTHEON HB. 125 SERIES 9. BOEING 707 SEE LIST List dated 24th January. configurations shall be determined 10027602 MAX-VIZ Inc. P- FAA STC ST01523LA F900EX, MF50, MF900 EASA Validation of FAA STC This design change is also applicable on the Prior to installation of this modification it 13.10.2009 EASA.IM.A.S.02776 ST01523LA:Installation of Max-Viz Enhanced Mystere Falcon 50EXdesignation as defined on must be determined thatthe Vision System (EVS) 1000 in accordancewith EASA TCDS.A.062 but limited to the interrelationship between this modification Master Drawing List Document number 3038- serialnumber aircraft MSN 286. For this MSN and any other previouslyinstalled 00025 Revision 5, dated14th October 2008 or 286 aircraft the applicable EASAFlight Manual modification and/ or repair will introduce later revisions approved by EASA in Supplement is the initial release of Docu no adverse effectupon the airworthiness accordance withEASA ED of the product. 10017126 MBH TECHNIC'S EASA.R.S.01214 SA 365 N S/N 6100 Installation of EMS cabin configuration, in This STC is limited to SA 365 N s/n 6100 and accordance with MBH Technic's STC file n° 01 can be installed only by MBH Technic's MBHT-05, original issue dated 29/03/2005, or technical staff in accordance with MBH later EASA approved revision. Technic's STC file n° 01 MBHT-05, original issue dated 29/03/2005, or later EASA approved revision. 04/01/2013 Page 328/462 27.02.2007
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10015807 MCCAULEY PROPELLER SYSTEMS EASA.IM.A.S.01875 FAA STC SA00798CH CESSNA FR-182 Installation of a McCauley Propeller Model FAA Approved Flight Manual Supplement, 08.06.2006 B3D36C431/80VSA-1 or B3D36C433/80VSA- Technical Report Number 874, dated August 1, and spinner assembly. 4, 1997, or later approved revision required.Lycoming engine model O-540- J3C5D is eligible with the McCauley Propeller Model B3D36C433/80VSA-1 (S/N FR18200001 through FR182000 10016128 MCCAULEY PROPELLER SYSTEMS EASA.IM.A.S.02322 FAA STC SA496CH BEECH 23 Installation of McCauley Propeller Model 1. Aircraft Specifications are the same as listed 22.05.2007 B3D36C429/82NPR-6 on Type Certification Data Sheet A1CE, except as follows:Propeller and Propeller Limits:Propeller: McCauley Constant Speed B3D36C429/82NPA-6Number of blades: 3 Blade Angels: At 30" station: Low 10. 10029619 MCCAULEY PROPELLER SYSTEMS P- EASA.IM.A.S.03127 FAA STC SA01511WI C400 (LC41-550FG) Installation of McCauley C447 As referred in limitations section of the AFM-S The installation of this modification by 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 interr 10017129 MECAER AVIATION GROUP S.P.A. EASA.R.S.01219 REV. 1 AB139/ AW139 AB139 VIP 28 P/N 6AB1KT003-001 Interior Configuration. This STC supersedes EASA STC EASA.R.S.01219. Approval of this change in type design applies only to those AB139rotorcraft previously equipped with EASA approved Installation of AgustaKit VIP PROVISION P/N 4G2520F00511. 06.04.2010 Prior to installation of this modification it 09.06.2010 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. 10017130 MECAER AVIATION GROUP S.P.A. EASA.R.S.01220 REV. 2 AW139 VIP 29 Interiors 10 seats P/N 6AB1KT004-001. 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. 16.07.2012 10017140 MECAER AVIATION GROUP S.P.A. EASA.R.S.01242 REV. 1 AB139/ AW139 VIP 37 Interiors P/N 6AB1KT005-001: Cabin interiors modification. This STC supersedes EASA STC EASA.R.S.01242. 10017149 MECAER AVIATION GROUP S.P.A. EASA.R.S.01252 REV. 2 A109S, AW109SP Cabinet Installation P/N 6A10AD001-001. Extension of the STC 10017149 to the AW109SP model that is part of thesame TC Number EASA.R.005 The change in type design applies only to those Prior to installation of this modification it 09.06.2010 AB139/AW139 Rotorcraftpreviously equipped must be determined thatthe with Agusta "Kit VIP Cabin Passenger interrelationship between this modification Provision P/N4G2520F00711". and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product. None Prior to installation of this modification the 01.03.2011 installer must determinethat the interrelationship between this modification and any otherpreviously installed modification will introduce no adverse effect uponthe airworthiness of the product. 10017150 MECAER AVIATION GROUP S.P.A. EASA.R.S.01253 REV. 1 AB139/ AW139 CD Player Installation P/N 6AB1EL017-001 the The change in type design applies only to those Prior to installation of this modification it 09.06.2010 change consists in theinstallation of a CD AB139 Rotorcraft previously equipped with must be determined thatthe Player into passenger cabin. This STC Agusta provision P/N 3G2520A00311 interrelationship between this modification supersedes EASA STC EASA.R.S.01253. and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product. 10017151 MECAER AVIATION GROUP S.P.A. EASA.R.S.01254 REV. 1 AB139/ AW139 SAT-COM Installation P/N 6AB1EL018- 001The change consists in the installation of a Satellite Telephone Systemon passenger cabin. This STC supersedes EASA STC EASA.R.S.01254. The change in type design applies only to those AB139 Rotorcraft previously equipped with Agusta SAT-COM provision P/N 3G2310F00411 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. 04/01/2013 Page 329/462 19.06.2006
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04/01/2013 Page 1/462 - EASA

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