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 10038517 FIELD AVIATION EAST, LTD. TCCA STC SA05-8 DHC-8-202 Max. Gross Takeoff Weight Increase to 37.300 None Prior to installation of this modification it 22.02.2012 lbsTCCA STC SA05-08, Issue 1 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. 10038533 FIELD AVIATION EAST, LTD. TCCA STC O-LSA11-177/D DHC-8-202 Cabin Drop Down Oxygen System Removal and Cabin Interior RefurbishmentTCCA STC O-LSA11-177/D, Issue 1 10039284 FIELD AVIATION EAST, LTD. REV. 1 TCCA STC O-LSA11-147/D DHC-8-202 Air Iceland Avionics UpgradeTCCA STC O- LSA11-147/D, Issue 1 10017035 FILTRATION DEVELOPMENT CORPORATION EASA.IM.R.S.01459 FAA STC SR01616SE SIKORSKY S-76A SIKORSKY S-76A++ SIKORSKY S-76C SIKORSKY S-76C+ Installation of an Engine Air Filter System for Sikorsky S-76 models, A+, A++ and C & C+ The modification is limited to Serial numbers 445, 446. Prior to installation of this modification it 23.02.2012 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. The modification is limited to Serial numbers Prior to installation of this modification it 03.05.2012 445, 446.Universal UNS-1E(w) Flight must be determined thatthe Management Systems are approved for IFREn- interrelationship between this modification route, Terminal and Non Precisions approach and any other previouslyinstalled operations. modification and/ or repair will introduce no adverse effectupon the airworthiness of the product. 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. 10014229 FINNAIR OYJ EASA.A.S.01392 BOEING MD 11 MD11 Cabin Crew Rest Area Emergency evacuation procedures, including the emergency evacuation of an incapacitated occupant from the Crew Rest Area, must be established. All of these procedures must be transmitted to the operator for incorporation into their training programs and ap 10016090 FIREWALL FORWARD TECHNOLOGIES LLC 10016691 FIREWALL FORWARD TECHNOLOGIES LLC 10016696 FIREWALL FORWARD TECHNOLOGIES LLC 10016697 FIREWALL FORWARD TECHNOLOGIES LLC EASA.IM.A.S.02277 FAA STC SA01435LA Installation of engines, modified with a Firewall Forward Technologies, LLC modified camshaft, into aircraft listed on the EASA approved ATL EASA.IM.E.S.01005 FAA STC SE00584DE Installation of modified Oil Fitter Adapter, an increased opening pressure spring for filter bypass, and modified filter stud in accordance with Firewall Forward Technologies. Inc. Master Document List No. FFT-MDOCLST- OILSTUD-001, Rev. B, dated August 8, 2 EASA.IM.E.S.01010 FAA STC SE01436LA Installation of Firewall Forward Technologies, LLC modified camshaft in accordance with Master Drawing List FWF-MDL-ST9721 LA-E, revision G, dated 2/14/03 or later FAA approved revision. 1. This installation must be done concurrently with EASA STC No. EASA.IM.E.S.01010, which modifies the engine.2. Regardless of the EASA Approved Type List (ATL), installation is only approved if the Airplane Type / Variant itself is EASA approved.3. Compatibility of this design change with previously approved modifications must be determined by the installer.If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written eviden This installation must be done concurrently with EASA STC No. EASA.IM.A.S.02277, which modifies the airplane installation.Compatibility of this design change with previously approved modifications must he determined by the installer. The installation shoul EASA.IM.E.S.01011 REV. 1 FAA STC SE00590DE Installation of a Lubricated Camshaft in 1. All engine installation criteria and limitations accordance with Master Drawing List FFT-MDL- are unchanged and remain in effect. ST3370DE-E, Revision IR dated September 9, Installation of engines modified by this STC 2005, FAA approved September 26, 2005, or must be in accordance with the original aircraft later FAA approved revision. installation criteria.2. Instructions for Continued Airworthiness, Firewal 10015970 FIRST AIR MAINTENANCE SERVICES EASA.IM.A.S.02121 SA06-39 AEROSPATIALE ATR 42-300 AEROSPATIALE ATR 42-320 AEROSPATIALE ATR 72-101 AEROSPATIALE ATR 72-102 AEROSPATIALE ATR 72-201 AEROSPATIALE ATR 72-202 Installation of Dual SAGEM F227 APIRS Attitude and Heading Reference System This STC is approved only for the aircraft modelsATR 42-200 / 300 / 320 / 400 / 500ATR 72-101 / 102 / 201 / 202 / 211 / 212 / 212 Afor those serial numbers fitted with the Honeywell AH600 AHRS as per originally manufactured and delivered by ATR (Type Desig 04/01/2013 Page 218/462 05.02.2009 15.08.2006 12.02.2007 18.01.2007 06.02.2007 05.02.2007 16.01.2007
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10017203 FISCHER + ENTWICKLUNGEN EASA.R.S.01352 BELL 427 Installation of floor mounted F+E Medical Seats 230/305 into Bell 427 cabin by use of installation racks attached to forward and aft cabin bulkhead fittings 20.07.2007 10015484 FLIGHT ENVIRONMENTS INC EASA.IM.A.S.01244 FAA STC SA01318LA BEECH 390 Installation of thermal/accoustic insulation kit 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. 26.07.2005 10015709 FLIGHT STRUCTURES, Inc. EASA.IM.A.S.01702 FAA STC ST02944AT B777-200, B777-300 Installation of Cabin Wireless Local Area Airworthines Limitations Section of the 20.07.2006 Network (CWLAN) Distribution System Instruction for Continuous Airworthiness, document numbers F44-0246, revision A, dated 20thOctober 2004 or R44-0406, revision IR, dated 23rd June 2005 or later FAA approved revisions 10015719 FLIGHT STRUCTURES, Inc. EASA.IM.A.S.01717 FAA STC ST01729SE B747-400 Business Class Seat Installation Boeing Service Bulletin 747-25-3420 dated June 13 2006 must be installed concurrently with this STC. 17.01.2007 10015720 FLIGHT STRUCTURES, Inc. EASA.IM.A.S.01719 REV. 3 FAA STC NO. ST01849SE 777-200 Business Class Seat Installation Boeing Structural Compliance summary Prior to installation of this modification it 02.02.2012 Report Document DLR-36718 revisionNew must be determined thatthe dated 17 March 2008 must be accomplished interrelationship between this modification concurrently with this STCBoeing Structural and any other previouslyinstalled Compliance Summary Report Document DLR- modification and/ or repair will introduce 36718 RevisionNew dated 17 March 2008 no adverse effectupon the airworthiness must be accomplishe of the product. 10016319 FLIGHT STRUCTURES, Inc. EASA.IM.A.S.02627 REV. 3 FAA STC ST01950SE B777-200 Remove EWIS limitation for EASA STC No. EASA.IM.A.S.02627 Rev 1 - Door 1Overhead Flight Crew Rest Installation The Boeing Service Bulletin 777-25-0429 dated 15 October 2008 must beaccomplished concurrently with this STC for the serial numbers listed onthe FSI top Collector A700000-001 revision C dated 8 December 2008The Main deck seat arrangement must be installed 10016564 FLIGHT STRUCTURES, Inc. EASA.IM.A.S.02955 FAA STC ST00386SE BOEING 747-200 This design change relocates the E/E Bay This STC can only be installed in aircraft with Acces Hatch on the main deck floor and FAA STC SA2725CE-D or STC ST00255WI-D Installs Gari o Handling System Provisions for a or STC ST00252WI-D or STC ST00214SE 30pallet main deck cargo configuration per Flight Structures, Inc. installed. 10016610 FLIGHT STRUCTURES, Inc. EASA.IM.A.S.03030 REV. 2 FAA STC ST02004SE B777-200 Remove EWIS limitation for EASA STC No. EASA. IM.A.S.03030 - Door 3Overhead Attendant Rest Installation 10029094 FLIGHT STRUCTURES, Inc. P- EASA.IM.A.S.02978 10029964 FLIGHT STRUCTURES, Inc. P- EASA.IM.A.S.03045 10031815 FLIGHT STRUCTURES, Inc. P- EASA.IM.A.S.03215 REV. 1 FAA STC ST02051SE B777-200 Remove EWIS limitation for EASA STC No. 10029094 - First Class SeatInstallation REV. 1 FAA STC ST02060SE B747-400 Amendment of STC 10029964 in order to remove EWIS Limitations and updatethe MDL reference FAA STC ST02038SE A330-300 Installation of an Interior Reconfiguration in A330-300 Series aircraft 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 07.10.2010 18.09.2008 The Main deck seating arrangement must be Prior to installation of this modification it 07.10.2010 installed in accordance withBritish Airways must be determined thatthe drawing 3-302-342 revision 10 dated 12 interrelationship between this modification February 2009FSI STC 10016319 rev. 2 (FAA and any other previouslyinstalled STC number ST01950SE) for the FSI Door modification and/ or repair will introduce 1Overhead Flight Crew Rest Installation no adverse effectupon the airworthiness (OFCR) mus of the product Concurrent installation of EASA STC No. 10029095 (EASA Project No.P- EASA.IM.A.S.03043) is requiredConcurrent installation of EASA STC No. EASA.IM.A.S.01797 is required Concurrent Installation of EASA STC No. 10029975 is requiredConcurrent installation of FAA STC ST00720LA (EASA approved undergrandfather rights by CAA Airworthiness Approval Note No. 26656 dated 8March 1999) is required Prior to installation of this modification it 04.10.2010 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 Prior to installation of this modification it 04.10.2010 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 Not applicable Concurrent installation of Delta Engineering Supplemental TypeCertificate EASA STC 10031836 is required Concurrent installation of AmSafe, Inc. Supplemental Type CertificateEASA STC 10031808 is required Prior to installation of this modification it must be 04/01/2013 Page 219/462 17.09.2010
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04/01/2013 Page 1/462 - EASA

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