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 10015423 TEXAS SKYWAYS, INC. EASA.IM.A.S.01154 FAA STC SA09133SC CESSNA 182 Installation of Teledyne Continental Motors IO- The approval is only valid in combination with 07.07.2006 CESSNA 182A 550-F engine and Hartzell or McCauley the installation of STC EASA.A.S.01374 CESSNA 182B Propeller in acc. with Texas Skyways Spec. (Gomolzig GmbH, Germany) CESSNA 182C TS0028, Rev. 1, or later approved Revision CESSNA 182D CESSNA 182E CESSNA 182F CESSNA 182G CESSNA 182H CESSNA 182J CESSNA 182K CESSNA 182L CESSNA 182M CESSNA 182N CESSNA 182P CESSNA 182Q CESSNA 182R CESSNA F182-P CESSNA F182-Q and TS0034 10015424 TEXAS SKYWAYS, INC. EASA.IM.A.S.01155 FAA STC SA10070SC CESSNA 180 Installation of Hartzell 3-blade Propeller in acc. The approval is only valid with latest EASA 07.07.2006 CESSNA 180A with Texas Skyways Doc. 5016-0000, Rev. E, approved Noise Certificate CESSNA 180B CESSNA 180C CESSNA 180D CESSNA 180E CESSNA 180F CESSNA 180H CESSNA 180J CESSNA 180K CESSNA 182 CESSNA 182A CESSNA 182B CESSNA 182D CESSNA 182E CESSNA 182F CESSNA 182G CESSNA 182H CESSNA 182J CESSNA 182K CESSNA 182L CESSNA 182M CESSNA 182N CESSNA 182P CESSNA 182Q CESSNA 182R CESSNA 185 CESSNA 185A CESSNA 185B CESSNA 185C CESSNA 185D CESSNA 185E CESSNA 207 or later approved Revision 04/01/2013 Page 446/462
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10015425 TEXAS SKYWAYS, INC. EASA.IM.A.S.01156 FAA STC SA09964SC CESSNA 180 Installation of engine mount heat shields in acc. 07.07.2006 CESSNA 180A with Texas Skyways Doc. 5018-101, dated 12 CESSNA 180B CESSNA 180C CESSNA 180D CESSNA 180E CESSNA 180F CESSNA 180G CESSNA 180H CESSNA 180J CESSNA 180K CESSNA 182 CESSNA 182A CESSNA 182B CESSNA 182C CESSNA 182D CESSNA 182E CESSNA 182F CESSNA 182G CESSNA 182H CESSNA 182J CESSNA 182K CESSNA 182L CESSNA 182M CESSNA 182N CESSNA 182P CESSNA 182Q CESSNA 182R CESSNA F182-P CESSNA F182-Q Oct 2001, or later approved Revision 10016688 TEXAS SKYWAYS, INC. EASA.IM.E.S.01000 FAA STC SE09131SC Removal of fuel injection system and induction Approval of this change in type design applies 06.04.2006 system and installation of carburetor in to the above engine model only. Compatibility accordance with Texas Skyways, Inc. of this modification with previously approved Specification TS0030, dated 01 May 1995 or modifications must be determined by the FAA later approved revision, based on FAA installer. A copy of this Certificate must be Supplemental Type Certificate Number SE09131SC maintained as part of the perma 10038267 THALES AVIONICS Inc. REV. 1 FAA STC NO. ST02411LA 777-200 In-Flight Entertainment (IFE) System Concurrent installation of the following STCs Prior to installation of this modification it 03.02.2012 Installation are required for theinstallation of this STC:1) must be determined thatthe Flight Structures, Inc. EASA STC No. interrelationship between this modification 10015720, Business Class SeatInstallation.2) and any other previouslyinstalled Northwest Aerospace Technologies, Inc. modification and/ or repair will introduce EASA STC No. 10038268 (EASAProject No. no adverse effectupon the airworthiness 00 of the product. 10041205 THALES AVIONICS Inc. FAA STC ST02431LA A321-211, A321-212, A321-213, A321-231, A321-232 Installation of Thales Avionics IFS TopSeries In- This STC must be installed in conjunction with Flight Entertainment(IFE) System EASA STC 10040704 -Aerospace Engineering Solutions (AES) - Introduction of Twin Class CabinConfiguration 10042547 THALES AVIONICS Inc. A321-211,-212,-213,-231,-232 Installation of Thales Avionics IFS TopSeries In- This STC must be installed in conjunction with Flight Entertainment(IFE) System. 10042295 THE BOEING COMPANY EASA.IM.A.S.03158 FAA STC ST01697SE B737-700/-800 Lower Cabin Altitude (LCA) modification: cabin altitude reversion to 6,500 ft in lieu of 8,000 ft at 41,000 ft flight altitude. Modification in accordance with Boeing's "Master document listfor Lower Cabin Altitude modification" D926A200. EASA STC 10040704 -Aerospace Engineering Solutions (AES) - Introduction of Twin Class CabinConfiguration. Prior to installation of this modification it 29.08.2012 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. Prior to installation of this modification it 07.12.2012 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. See EASA Approved Annex 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. A sur 22.11.2012 04/01/2013 Page 447/462
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