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 10016005 AVIATION FABRICATORS / CENTRAL EASA.IM.A.S.02168 FAA STC ST01139WI CESSNA 560 Installation of a 39-inch or a 45-inch two-place The STC covers only installation of parts divan or a 24-inch one-place divan per Aviation contained in the Description sectionUpholstery, 13.09.2006 Fabricators STC Data Package, AF-342, Rev covers, aisle width, oxygen, seat belts are not A, dated 12, June, 2003 and stamped "FAA Approved" with an approval date of October 22, 2003 or later approved revisi covered 10015576 AVIATION FABRICATORS, Inc. EASA.IM.A.S.01487 REV. 1 FAA STC SA2629CE 200, 200C, 200CT, 200T, 300 300LW, B200, B200C, B200CT B200GT, B200CGT B200T, B300, B300C Installation of two place side-facing divan. 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 1. This STC must be installed per 08.10.2009 Aviation Fabricators drawing D-10265,no revision or later approved revision on airplanes manufactured after12 December 1986, with nine or fewer passenger seats, including thedivan. 2. For other divan installation, Aviatio 10029817 AVIATION FABRICATORS, Inc. FAA STC ST01572WI 400 Beechjet 400 Cabin Configuration. 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. 22.04.2010 10029869 AVIATION FABRICATORS, Inc. FAA STC NO. SA00961WI PA-31-325, PA-31-350 PA-31P, PA-31T, PA-31T1 PA-31T2, PA-31T3, PA-31 PA-42, PA-42-720, PA-42-1000 Stretcher Installation per Aviation Fabricators, Inc. STC Drawing List,Doc. No. AF-204 10031917 AVIATION FABRICATORS, Inc. FAA STC SA2818SW 441 Installation of 1, 2 or 3 place side seating divans in accordance withFAA STC SA2818SW 10032446 AVIATION FABRICATORS, Inc. FAA STC SA2774CE 1. 200, 200C, 200CT, 200T 1. A200, A200C, A200CT, B200 1. B200CT, B200T, 300, 300LW 2. B200C, B200CGT, B200GT 2. B300, B300C 10032903 AVIATION FABRICATORS, Inc. FAA STC REF SA4157SW SEE EASA APPROVED MODEL LIST Installation of Passenger Seats with Hinged Backrest. Installation of one, two, or three place side facing seat (frame only). The installer is responsible for ensuring that the installation complieswith any supplemental oxygen requirements as required for operation The installation of this modification by 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 27.04.2010 none thatthe interrelationship b 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. 22.09.2010 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. 08.11.2010 None This STC only approves the installation of 07.12.2010 the parts contained in theabove section "associated technical documentation". The requirements forthe aisle width, passenger oxygen system, seats and safety belts, andupholstery coverings will require a separate a 10015323 AVIATION PARTNERS BOEING EASA.IM.A.S.00279 REV. 3 FAA STC ST00830SE BOEING 737-700 Installation of Aviation Partners Boeing 1. Subject to compliance with the provisions 30.06.2008 BOEING 737-800 Winglets in accordance with the following of Part 21 Subpart E, this STC and associated BOEING 737-900 documents:- APB Document List AP37.7- data shall remain valid until surrendered, E620 Rev. A (737-700)- APB Document List withdrawn or otherwise terminated.2. If AP37.1- E620 Rev. A (737-700IGW)- APB transfer of this Certificate is requested under 10015659 AVIATION PARTNERS BOEING EASA.IM.A.S.01636 REV. 5 FAA STC ST01518SE B757-200, -300 Document List AP37.8- E620 Rev. A (737-800)- Part 21A.116 the STC will be APB Documen Install of Aviation Partners Boeing Winglets on The Partial Wing Retrofit Installation (300-1 Kit) Prior to installation of this modification it 11.04.2011 B757-200 and B757-300Aeroplanes is approved for RollsRoyce RB211-535 must be determined thatthe powered a/c. 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 90/462
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10016394 AVIATION PARTNERS BOEING EASA.IM.A.S.02723 REV. 3 FAA STC ST01920SE BOEING 767-300, -300F Installation of Aviation Partners Boeing Operational/ Performance limitations are Prior to installation of this modification it 07.01.2011 Winglets on Boeing B767-300 and-300F a/c. defined within the AFMsupplement. This STC must be determined thatthe is approved for a/c equipped with General interrelationship between this modification Electric CF6-80C2series engines or Pratt and and any other previouslyinstalled Whitney PW 4000 series engines with modification and/ or repair will introduce noengine strut vibration isolators installed only no adverse effectupon the airworthiness of the product. 10029056 AVIATION PARTNERS BOEING EASA.IM.A.S.02838 FAA STC ST01219SE BOEING 737-500 15.07.2009 10015403 AVIATION PARTNERS, INC. EASA.IM.A.S.01113 FAA STC ST01411SE BAE 125 SERIES 800A Installation of Winglets, associated changes in Installation of this STC on Model Hawker 26.10.2005 BAE 125 SERIES 800B wing and Aileron structures and related 800XP is limited to Aircraft equipped with the HAWKER 800 XP systems changes on Raytheon Aircraft Honeywell DFZ-800 (SPZ-800 avionics) Company Model Bae 125 Series 800A, 800B autopilot, the Collins 85/86 (FCC-86E avionics) and Hawker 800XP Aircraft, in accordance auto pilot and Collins Pro line 21 (FGC-300 with FAA STC ST01411SE avionics) autopilot, for Category I app 10028844 AVIATION PARTNERS, INC. EASA.IM.A.S.02043 FAA STC ST01987SE DASSAULT FALCON 2000 DASSAULT FALCON 2000EX SERIES 10038665 AVIATION PARTNERS, INC. REV. 1 FAA STC ST02188SE MF900, F900EX FAA STC ST02188SE: Installation of blended Applicable to MF900 aircraft orApplicable to winglet on Dassault Falcon900 Series airplanes MF900 aircraft fitted with modification M1975 orApplicable to Falcon 900EX aircraft orApplicable to Falcon 900EX fitted with modifications M3083 or M4000 10015248 AVIATION SERVICE A.S. EASA.A.S.03687 LETECKE ZAVODY L 410 UVP-E Installation of EGPWS Mark VI. 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. 10029324 AVIATION SERVICE A.S. P-EASA.A.S.03854 L 200 A, L 200 D Installation of Aspen EDF-1000 "PRO" and EFD-1000 "PILOT", GNS 430W, GTX330, KR 87, KN 62A and ELT ME406 systems. 10030602 AVIATION SERVICE A.S. L410 UVP-E, L410 UVP-E9, L410 UVP-E20 TCAS II CAS67A, Mode S transponder MST67A, and Air Data Display UnitAD32 installation to comply with regulation requirements. 10031903 AVIATION SERVICE A.S. 407 Installation of alternate static port for VFR night operation 10033022 AVIATION SERVICE A.S. AN-26B An-26 Aircraft Upgrade; TCASII CAS-67A, Mode S Transpon. MST-67A andKT73, EGPWS Mk-VI, NAV/COMM KX165A, GPS155XL, Audio panel KMA28, WxRadar ART2000, MFD KMD540, ADF KR87, DME KN63, Air Data Display AD32,RAlt KRA405B, Airspeed Ind. LUN110, ELT C406-2; Steep approach Operation with Winglets installed is not approvedHUD/CATIII Operation with Winglets installed is not approvedPrior to installation of this modification it must be determined thatthe interrelationship between this modification and any other p None. Prior to installation of this modification the installer must determinethat the interrelationship between this modification and any otherpreviously installed modification will introduce no adverse effect uponthe airworthiness of the 08.05.2009 08.08.2012 24.11.2008 18.03.2010 None product.The installatio None 24.06.2010 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 21.09.2010 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 15.12.2010 10017094 AVIATION SUPPORT GmbH EASA.R.S.01006 EUROCOPTER DEUTSCHLAND Installation of a Gas Detection System CHARM 13.02.2007 BO-105 with a laser scanner 10017159 AVIATION SUPPORT GmbH EASA.R.S.01267 SCHWEIZER AIRCRAFT 269A SCHWEIZER AIRCRAFT 269B SCHWEIZER AIRCRAFT 269C SCHWEIZER AIRCRAFT 269C-1 SCHWEIZER AIRCRAFT 269D Installation of Clipboard/Tablet-PC rack -- 30.01.2007 04/01/2013 Page 91/462
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04/01/2013 Page 1/462 - EASA

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