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 10015395 NORTHWEST AEROSPACE EASA.IM.A.S.01096 BOEING 757-200 Installation of ELS/EHS S system Upgrade This STC is approved only for the product 15.08.2005 TECHNOLOGIES In 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. 10028415 NORTHWEST AEROSPACE P-EASA.A.S.03966 REV. 1 A320-232 Interior Reconfiguration and In Flight None Prior to installation of this modification it 05.08.2010 TECHNOLOGIES In Entertainment (IFE) Installationon Etihad must be determined thatthe Airways A320-232 Aircraft Revision of the interrelationship between this modification EASA 10028415 to remove EWIS limitation and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product. 10029095 NORTHWEST AEROSPACE TECHNOLOGIES In 10029975 NORTHWEST AEROSPACE TECHNOLOGIES In 10030495 NORTHWEST AEROSPACE TECHNOLOGIES In 10031457 NORTHWEST AEROSPACE TECHNOLOGIES In 10032214 NORTHWEST AEROSPACE TECHNOLOGIES In 10038268 NORTHWEST AEROSPACE TECHNOLOGIES In 10038505 NORTHWEST AEROSPACE TECHNOLOGIES In P- EASA.IM.A.S.03043 P- EASA.IM.A.S.03214 FAA STC ST02052SE B777-200 First Class Cabin Upgrade - BA 777-200 Aircraft Concurrent installation of EASA STC No. 10029094 (EASA Project NoP- EASA.IM.A.S.02978) is required.Concurrent installation of EASA STC No. EASA.IM.A.S.01797 is required.This modification may not be installed after 30 August 2010 unless (1)previously approve FAA STC ST10594SE-T B747-400 First Class Cabin Upgrade BA 747-400 aircraft Concurrent installation of EASA STC 10029964 is required.This modification may not be installed after 30 August 2010 unless (1)previously approved electrical wiring interconnect system (EWIS)instructions for continued airworthiness (ICA) have been evaluate P-EASA.A.S.03958 A319-132 Interior Reconfiguration and In Flight Entertainment (IFE) Installationon Etihad Airways A319-132 Aircraft FAA STC ST02079SE B777-300 First and Business Class Cabin Interior - BA 777-300 aircraft A320-232 Cabin Interior Reconfiguration and In Flight Entertainment (IFE)Modifications on Etihad Airways A320-232 Aircraft FAA STC NO. ST02412LA 777-200 First and Economy Class Cabin Interior - BA 777-200 Aircraft Prior to installation of this modification it 03.03.2010 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 07.05.2010 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. 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. 18.06.2010 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. 17.08.2010 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 18.10.2010 Concurrent installation of the following STCs are required for theinstallation of this STC:1) Flight Structures, Inc. EASA STC 10015720, Business Class SeatInstallation.2) Thales Avionics, Inc. EASA STC No. 10038267 (EASA Project No.0010011945), Passenger Prior to installation of this modification it 02.02.2012 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. FAA STC ST02195SE B747-400 Installation of a IMS RAVE In-flight Entertainment System into theeconomy class passenger seats of a Boeing 747-400 aircraft in accordancewith Northwest Aerospace Technologies Inc. Master Drawing ListN0374- D10, Rev. J dated December 27, 2011 or later appro None. None. 22.02.2012 04/01/2013 Page 346/462
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10039202 NORTHWEST AEROSPACE REV. 1 B747-400 B747-400 Cabin re-configuration in accordance The use of the baby basinet is not permitted None 07.05.2012 TECHNOLOGIES In with Northwest AerospaceTechnologies Inc. unless a "Remove beforeTaxi, Take-off and Master Drawing List N0375-D10 Rev. A dated Landing" placard is installed either on the April 12,2012 babybassinet or on the surface on which the baby bassinet is mounted. Theuse of cabin crew procedures to show compliance with 10040082 NORTHWEST AEROSPACE TECHNOLOGIES In 10040295 NORTHWEST AEROSPACE TECHNOLOGIES In 10041628 NORTHWEST AEROSPACE TECHNOLOGIES In 10015367 NORTHWEST COMPOSITES EASA.IM.A.S.00763 FAA STC ST01565SE BOEING 737-300 BOEING 737-400 10015740 NORTHWEST COMPOSITES EASA.IM.A.S.01764 FAA STC ST00867SE DC-9-82 DC-9-83 10015741 NORTHWEST COMPOSITES EASA.IM.A.S.01765 FAA STC ST00868SE DC-9-82 (CF6) DC-9-83 (MD-83) 10017243 NSE INDUSTRIES S.A. EASA.R.S.01440 AS365N2, AS365N3 SA365N, SA365N1 B747-400 Interior Reconfiguration of VAA 747-400 A/C serial numbers: 30885, 32337, 32338, Aircraft: Cabin Configurationand Passenger Amenities Upgrade and Standardization in accordance withNAT Master Data List N0377- D10 Rev. B , dated May 22, 2012 32339, 32340, 28757 and 29406. B777-300ER N0401: Certification of Deployment of In-Seat Video Monitors DuringTaxi, Take-Off and Landing - Business Class Seats on Cathay PacificB777-300(ER) Aircraft 777-300ER N0419 Cabin Interior Modifications on Jet Airways Boeing 777-300ERAircraft Maintenance Manual Supplement, 12.06.2012 Northwest Aerospace Doc. N0377- D71Revision -, 20 February, 2012 or later approved revision is requiredwith this installation. The Instructions for Continued Airworthiness, Electrical WiringInterconnect System Instructions for Limited to 777-300ER as per EO 20N00968 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. 22.06.2012 Stowage bin Extension. 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. Stowage Bin ExtensionModification to 1. Aircraft listed on Master Drawing List overhead stowage bin located in the passenger A075000 rev. F dated 20th January or later cabin in order to extend the bins for aircraft approved revision.2. This approval of this originally equipped with Heath-Techna Interiors change in type design applies to the above stowage bins. model aircraft only.3. This approval should not be extended to other aircraf Stowage Bin ExtensionModification to 1. Aircraft listed on Master Drawing List overhead stowage bin located in the passenger A074000 rev. J dated 3rd November 2005 or cabin in order to extend the bins for aircraft later approved revision.This approval of this originally equipped with C&D Interiors stowage change in type design applies to the above bins.FAA STC ST00868SE issue on 21st June model aircraft only.This approval should not be 2001 extended to other aircaft of thi Installation of BRITE SAVER 2 Usage Monitoring System This STC is a revision of EASA.R.S.01440 and covers software upgrade andapplicability modification. 10036630 NSE INTEGRATIONS ATR 42-300 Modification in ATR42-300 MSN 049's calibration test bench 10015792 O&N AIRCRAFT MODIFICATIONS, INC. EASA.IM.A.S.01851 FAA STC SA615NE CESSNA 172F CESSNA 172G CESSNA 172H CESSNA 172I CESSNA 172L CESSNA 172M CESSNA 172N CESSNA 172P Installation of an 18 gallon fuel tank in the aft baggage compartment, and fuel transfer system. 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 17.06.2005 28.03.2006 16.02.2006 None Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification will introduce no adverse effect upon theairworthiness of the product. The approval holder s 21.12.2012 This STC is limited to ATR42-300 serial number aircraft MSN 049 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. Prior to installation of this modification it 28.09.2011 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 347/462 29.08.2006
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04/01/2013 Page 1/462 - EASA

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