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 10034119 ROEDER PRAEZISION GMBH PIPER PA-31-350 Provision for Camera Installation. None. This STC includes only the structural changes and the electrical powerbox. It does not include any installation of Equipment (e.g.Laserscanner, Computer, Cameras).Prior to installation of this modification it must be determined thatthe interrelationship be 08.03.2011 10039546 ROEDER PRAEZISION GMBH TU206F Installation of an additional Alternator with Battery for MissionPurposes 10039554 ROEDER PRAEZISION GMBH 172S Installation of provision for the installation of a camera in the lowerfuselage as described in description document 14576DE 5300 10 00D. 10015845 ROSE UPHOLSTERY, Inc. EASA.IM.A.S.01945 SA10188SC BAE JETSTREAM 3201 Cabin Reconfiguration - 12 Passenger Executive Interior 10015376 ROSEMOUNT AEROSPACE, Inc. EASA.IM.A.S.01049 FAA STC ST02175CH BOEING 747-400 Installation of Rosemount Aerospace 8400M Series Cockpit Door Surveillance System 10015857 ROSEMOUNT AEROSPACE, Inc. EASA.IM.A.S.01961 FAA STC ST00971SE-D BOEING 737-300 BOEING 737-400 BOEING 737-500 10015899 ROSEMOUNT AEROSPACE, Inc. EASA.IM.A.S.02020 FAA STC ST02368CH BOEING 737-300 BOEING 737-400 BOEING 737-500 BOEING 737-600 BOEING 737-700 BOEING 737-800 BOEING 737-900 10016410 ROSEMOUNT AEROSPACE, Inc. EASA.IM.A.S.02742 REV. 3 FAA STC ST02649CH A319-111/-112/-113/-114/-115 A319-131/-132/-133 A320-111/-211/-212/-214 A320-231/-232/-233 A321-111/-112/-131 A321-211/-212/-213/-231/-232 Installation of the Rosemount Aerospace Coockpit Door Surveillance system (CDSS). Installation of Rosemount Aerospace Cockpit Door Surveillance System (CDSS) in accordance with Rosemount Aerospace MDL, Doc No. D06400594, Revision B, dated December 29, 2006, or later EASA approved revision. Installation of Rosemount Aerospace 8700C2- 4 Laptop Docking Station -Electronic Flight Bag (EFB) System Provisions.A319/ A320 / A321 Series 8700C2-4 Laptop Docking Station (LDS) -Electronic Flight Bag (EFB) System Provisions. Revision of the EASA STC 10016 10016424 ROSEMOUNT AEROSPACE, Inc. EASA.IM.A.S.02762 FAA STC ST02712CH BOEING 747-400 Installation of Rosemount Aerospace 8700C2- 6 Series Laptop Docking Station (LDS) - Electronic Flight Bag (EFB) Systems Provisions in accordance with Rosemount Aerospace Master Data List, Doc. No. D06402649 Revision C, dated April 3, 2009 or 10016617 ROSEMOUNT AEROSPACE, Inc. EASA.IM.A.S.03044 REV. 2 FAA STC ST02675CH A340-211, -212, -213 A340-311, -312, -313 A340-541, -642 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. 10.05.2012 Installer must check availability of EASA- approval for one or morereferenced STC when airplane is modified per that / those STC(s).This STC is limited to S/N 172S8186.This STC provides instructions only for the installation of theprovision for a camera. Fu 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. - Compatibility of this design change with other previously approved modifications must be determined by the installer.- In accordance with Flight Manual Supplement, Rosemount Aerospace Doc No D06400184, Rev A, FAA approved January 4th, 2007, or later ap The installation of this modification by 10.05.2012 third persons is subject towritten permission of the approval holder and disposal of the approvedappropriate documentation. Prior to installation of this modification it must be determined thatthe interrelationship 11.04.2006 06.10.2005 20.04.2006 06.02.2007 Not applicable 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 18.11.2010 1. FAA approved Airplane Flight Manual Supplement, Rosemount Aerospace Doc. No. D06402687, Revision A, approved April 2, 2009 orlater FAA approved revision, is required on board of the modified aircraft.2. This installation approval does not include 23.04.2009 later FAA appro Installation of Rosemount Aerospace 8700C2- This installation approval does not cover the Prior to installation of this modification it 26.08.2010 3 Laptop Docking Station -Electronic Flight Bag Electronic Flight Bagcomputers, only the must be determined thatthe (EFB) System Provisions Revision of the EASA Electronic Flight Bag mounting and wiring. interrelationship between this modification STC 10016617, Rev. 1 to remove EWIS Theoperational approval of the Electronic Flight and any other previouslyinstalled Limitation Bag computers shouldfollow the guidance in modification and/ or repair will introduce the Temporary Guidance Leaflet TGL no adverse effectupon the airworthiness of the product 10016655 ROSEMOUNT AEROSPACE, Inc. EASA.IM.A.S.03104 BOEING MD 11F Installation of Rosemount Aerospace 8700C2- 1) Prior to installation of this modification the 8 Series Laptop Docking Station (LDS) - installer must determine that the Electronic Flight Bag (EFB) System Provisions interrelationship between this modification inaccordance with Rosemount Aerospace andany other previously installed modification Master Data List, Doc. No. D06403165, will introduce no adverse effect upon the Revision D, dated April 3, 2009 or later FAA approv airworthiness of the product.2) FAA app 04/01/2013 Page 374/462 10.06.2009
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10026912 ROSEMOUNT AEROSPACE, Inc. P- REV. 1 FAA STC ST02743CH B737-600, -700, -800, -900 Validation of major change to FAA STC Not Applicable Prior to installation of this modification it 01.07.2011 EASA.IM.A.S.03087 concerning EFB 'Installation of8700A1-3 must be determined thatthe Electronic Flight Bag'The change to EFB STC interrelationship between this modification adds the following features:- implementation of and any other previouslyinstalled Display Module (DM) ON/OFF backlight- modification and / or repair will introduce connections to WOW and Door Open discretes no adverse effectupon the airworthiness of the product. 10027535 ROSEMOUNT AEROSPACE, Inc. P- EASA.IM.A.S.03159 10033819 ROSEMOUNT AEROSPACE, Inc. P- EASA.IM.A.S.02736 FAA STC ST02761CH 737-300, 400, 500 Installation of Rosemount 8700C2-7 Series Refer to limitations and conditions on FAA Laptop Docking Station (LDS) -Electronic Flight ST02761CH. Bag (EFB) System. Validation of FAA STC ST02761CH REV. 1 FAA STC ST02668CH 777-200, 777-200LR, 777-300 777-300ER, 777F 10041824 ROSEMOUNT AEROSPACE, Inc. FAA STC ST02944CH 777-200, 777-200LR, 777-300 777-300ER, 777F Prior to installation of this modification it 08.10.2009 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. Installation of Rosemount Aerospace 8700C2- This installation approval does not include the Prior to installation of this modification it 18.10.2012 1 Laptop Docking Station- Electronic Flight Bag Electronic Flight Bagcomputers. The must be determined thatthe (EFB) System Provisions operational approval of the Electronic Flight interrelationship between this modification Bagcomputers should follow the EASA and any other previouslyinstalled Operational Approval process; Any equipment modification and/ or repair will introduce that is connected to the aircraft electrical p no adverse effectupon the airworthiness of the product. Installation of an AC-DC Converter. Aircraft modification iaw Rosemount Aerospace Master Data List, Doc. No.D06408653 Configuration A requires concurrent installation of a systemor of equipment utilizing the DC power provided by the AC-DC powerconverter; Aircraft modification iaw Rosemount Prior to installation of this modification it 18.10.2012 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. 10016035 ROSEN SUNVISOR SYSTEMS LLC EASA.IM.A.S.02204 REV. 2 FAA STC SA4147NM BAE 125 SERIES 1000A BAE 125 SERIES 800A HAWKER 1000 HAWKER 800 XP HAWKER 850 XP HAWKER 900 XP Installation of Cockpit Sun Visors. 21.05.2008 10016661 ROSEN SUNVISOR SYSTEMS LLC EASA.IM.A.S.03124 FAA STC SA01838SE Installation of Sunvisor. 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.2. 23.04.2009 10026892 ROSEN SUNVISOR SYSTEMS LLC P- EASA.IM.A.S.03271 10027193 ROSEN SUNVISOR SYSTEMS LLC P- EASA.IM.A.S.03219 10031251 ROSEN SUNVISOR SYSTEMS LLC P- EASA.IM.A.S.03270 FAA STC SA2614NM 1. MYSTERE FALCON 200 2. MYSTERE FALCON 50 FAA STC SA00871SE SEE EASA APPROVED MODEL LIST FAN JET FALCON C, D, E, F, G EASA Validation of FAA STC SA2652NMCockpit Sun Visor Installation i.a.w. Rosen Drawing List No. RF 20-00DL, Revision D dated 14th November 2008 or later revisions approved byEASA i.a.w. EASA ED Decisions 2007/001/C and 2004/04/CF (or subsequentrevisions to EASA Validation of FAA STC SA2614NM:Cockpit Sun Visor Installation in accordance with Rosen Drawing List No.RF 50/200-00DL, Revision C dated 26th August 2009 or later revisionsapproved by EASA in accordance with EASA ED Decision 2004/04/CF (orsubsequent re 10033410 ROSEN SUNVISOR SYSTEMS LLC FAA STC SA3529NM DHC-6-100, -200, -300 Cockpit Sun Visor installation in accordance with FAA STC SA3529NM None 1) Prior to installation of this modification the installer mustdetermine that the interrelationship between this modification and anyother previously installed modification will introduce no adverse effectupon the airworthiness of the product. 2) The inst This EASA approval is also applicable to the Falcon 50EX version of theMF50 aircraft model as per this aircraft version definition described onEASA TCDS.A.062 19.08.2009 Prior to installation of this modification it 15.09.2009 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. Installation of Sunvisor None Prior to installation of this modification the 04.08.2010 installer must determinethat the interrelationship between this modification and any otherpreviously installed modification will introduce no adverse effect uponthe airworthiness of the product. The installati none If the holder agrees to permit another person to use this certificate toalter the product, the holder shall give the person written evidence ofthat permission.Prior to installation of this modification it must be determined thatthe interrelationship betwee 04/01/2013 Page 375/462 19.01.2011
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04/01/2013 Page 1/462 - EASA

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