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 10040010 HELI-ONE NORWAY AS REV. 2 EC225 LP Installation of LH or RH or both Vertical Day VFR Only; Flight into known icing None 29.10.2012 Reference Door. conditions prohibited;Category A operations prohibited;Operations requiring certification for Ditching prohibited;Power On VNE: 150 kts or lower as limited by PMV;Power Off VNE: 150 kts or lower as limited by PMVMax ai 10017036 HELI-ONE USA EASA.IM.R.S.01460 FAA STC SH8601SW BELL 230 Installation of EDZ-705 EFIS four tube flight instrument System. (This STC was classified as Basic by the FAA and is approved usingthe Post Type Validation Principles.) 10017042 HELI-ONE USA EASA.IM.R.S.01466 FAA STC SH5880SW REV2 BELL 230 Installation of SPZ-7000 DAFCS System. 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. 10016843 HELI-TRADE CORPORATION EASA.IM.R.S.01219 SR01592SE BELL 205A-1 BELL 205B BELL 212 BELL 214ST BELL 412 Installation and Maintenance of Goodrich Internal HoistFAA STC SR01592SE 10017279 HELI-UNION EASA.R.S.01525 AS 365 N GPS Stand alone BRNAV FREEFLIGHT TNL 2001. Approach plus I/O Installation In order to operate the internal hoist in the referenced airframes, the following provision kits must be installed:HOIST P/N BELL PROVISION KIT # BELL SERVICE INSTRUCTION # HELICOPTER S/N EFFECTIVITYHTC-42305A 205-706-091-1 BHT-205-SI-44 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. 10016727 HERITAGE AVIATION LIMITED EASA.IM.R.S.01028 FAA STC SR09407RC EUROCOPTER FRANCE EC 155 Installation of Forward and Aft Facing B1 Passenger Couch 10016768 HERITAGE AVIATION LIMITED EASA.IM.R.S.01099 FAA STC SR00530NY EUROCOPTER FRANCE EC 155 Installation of a Cocoon wall panel system 1. This STC is approved only for the product B1 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. 10017029 HERITAGE AVIATION LIMITED EASA.IM.R.S.01448 FAA STC SH7733SW MD HELICOPTERS 369E Installation of enlarged instrument paqnel and Not compatible with the MDHI optional centre MD HELICOPTERS 369FF slant console. This STC has been classified as seat installation. MD HELICOPTERS 500N “BASIC” by the FAA and has been approved MD HELICOPTERS 600N under the PTVP. 10017048 HERITAGE AVIATION LIMITED EASA.IM.R.S.01472 FAA STC SR09483RC MD HELICOPTERS 369E Heritage Aviation, Ltd. STC SR09483RC; 1. Applicable to MDHI 369E, 369FF, 500N MD HELICOPTERS 369FF Replacement Instrument Panel (including and 600N helicopters.2. Prior to installation MD HELICOPTERS 500N pedestal, shrouds and glare shield) on of this modification the installer must determine MD HELICOPTERS 600N applicable MDHI 369E, 369FF, 500N & 600N that the interrelationship between this helicopters. modification and any other previously installed modification will introduc 10017049 HERITAGE AVIATION LIMITED EASA.IM.R.S.01473 FAA STC SR09484RC MD HELICOPTERS 369E MD HELICOPTERS 369FF MD HELICOPTERS 500N 10017068 HERITAGE AVIATION LIMITED EASA.IM.R.S.01504 FAA STC SR09481RC MD HELICOPTERS 369E MD HELICOPTERS 369F MD HELICOPTERS 369FF MD HELICOPTERS 500N MD HELICOPTERS 600N Heritage Aviation, Ltd. STC SR09484RC; Chelton EFIS installation on applicable MDHI 369E, 369FF & 500N helicopters. 10016082 HOLLINGSEAD INTERNATIONAL EASA.IM.A.S.02266 FAA STC ST01879LA BOEING 747-400 SERIES Installation of B/E Aerospace Air Chiller P/N 470-1 1. Applicable to MDHI 369E, 369FF, 500N.2. Operation with the Chelton EFIS is limited to VFR only.3. (See limitations specified in RFM Supplement)4. Prior to installation of this modification the installer must determine that the interrelations Heritage Aviation, Ltd. STC SR09481RC; 1. Applicable to MDHI 369E, 369F, 369FF, Installation of nose shelf on applicable MDHI 500N and 600N.2. Prior to installation of this 369E, 369F, 369FF, 500N & 600N helicopters. modification the installer must determine that the interrelationship between this modification and any other previously installed modification will introduce no a 10016189 HOLLINGSEAD INTERNATIONAL EASA.IM.A.S.02418 FAA STC ST00740LA-D BOEING 737-300 Installation of Smoke Detection and Fire Suppression Systems Provisions, Lower Cargo Compartments. 10016262 HOLLINGSEAD INTERNATIONAL EASA.IM.A.S.02541 FAA STC ST00404LA-D BOEING 737-400 Installation of Smoke Detection and Fire Suppression Systems Provisions, Lower Cargo Compartments. This approval is limited to airplanes on which C&D Zodiac Pantry P/N C481001-101 has been installed in accordance with STC ST01880LA 04/01/2013 Page 272/462 13.05.2008 05.06.2008 03.10.2006 16.03.2009 20.07.2005 18.07.2005 01.04.2008 19.03.2009 19.03.2009 19.03.2009 23.01.2007 09.10.2007 14.01.2008
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10016300 HOLLINGSEAD INTERNATIONAL EASA.IM.A.S.02597 FAA STC ST02147LA BOEING 777-200 SERIES Installation of B/E Aerospace air Chiller P/N Applicable only to A/C with C&D Zodiac pantry 18.06.2008 470-1 installation P/N C801001-101 and C801001- 103 covered by FAA STC ST02144LA and EASA STC P-EASA.A.S.02421. 10016499 HOLLINGSEAD INTERNATIONAL EASA.IM.A.S.02861 FAA STC 01835LA BOEING 767-200 BOEING 767-300 10015343 HONEYWELL INTERNATIONAL INC. EASA.IM.A.S.00442 REV 3 FAA STC ST00705SE BOEING 747-400, 747-200 Installation of the Enhanced Ground Proximity Warning System on a Boeing 747-200/-400 aircraft. 10015348 HONEYWELL INTERNATIONAL INC. EASA.IM.A.S.00498 FAA STC ST01124SE BOEING 747-400 SERIES Installation of the Flight Data Acquisition Management System 10015371 HONEYWELL INTERNATIONAL INC. EASA.IM.A.S.01014 REV 1 SEE STC LIST Installation of Honeywell TFE731-3D-1H or TFE731-3DR-1H Turbofan Engines. 10015377 HONEYWELL INTERNATIONAL INC. EASA.IM.A.S.01051 REV 1 FAA STC NO ST02005CH-D LEARJET 55 Installation of Honeywell N1 Digital Electronic Engine Control (DEEC)Note: This revision reflects the transfer of STC EASA.IM.A.S.01051 from Garrett Aviation Services to Honeywell International Inc. 10015462 HONEYWELL INTERNATIONAL INC. EASA.IM.A.S.01209 FAA STC ST01298AT BOEING 767-200 SERIES BOEING 767-300 SERIES Installation of mounting provisions and electrical Prior to installation of this modification the provisions for electronic flight bags. 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. Installation of Flight Data Aquistion & Management System (FDAMS) with Mark II Aircraft Communication & Reporting System 1This 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.For Boeing B747-2001. 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 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. 1. Pitch & Roll Attitude is sampled one per second.2. Pneumatic power is sampled once every 4 seconds. 10015491 HONEYWELL INTERNATIONAL INC. EASA.IM.A.S.01253 FAA STC ST00961AT BOEING 757-200 SERIES (ACARS) Installation of Flight Data Acquisition and Management System (FDAMS), FAA STC ST00961AT. 10015547 HONEYWELL INTERNATIONAL INC. EASA.IM.A.S.01438 FAA STC SA3122SO BOEING 747 Honeywell International Inc. of Redmond, 1. Refer to Approval Report IVW/LTB/TCP- Washington, USA has applied for an STC to 05.5330542. This STC is approved only for cover the installation of a CAS81 Traffic the product configuration as defined in the Collision Avoidance System (TCAS) II with dual approved design data referred to in the TRA-67 Mode S transponders on Boeing 747- paragraph "Description". Compatibility with 100/200/SP Series aircraft. The FAA has iss other aircraft/engine configurations sha 10015572 HONEYWELL INTERNATIONAL INC. EASA.IM.A.S.01479 FAA STC SA00842WI-D BEECH 1900D Installation of the Honeywell Mark VI Enhanced AFMS 006-00875-0000 is required on-board Grounfd Proximity Warning System for operation with Beech 1900 D series 10015575 HONEYWELL INTERNATIONAL INC. EASA.IM.A.S.01485 FAA STC SA2726SO DC-9-80 (MD-80) SERIES Installation of CAS-81 TCAS II SystemFAA STC SA2726SO 10015685 HONEYWELL INTERNATIONAL INC. EASA.IM.A.S.01670 FAA STC SA01116WI-D PILATUS PC-12/45 Single or Dual Altimeters (FAA STC SA01116WI-D) 10015686 HONEYWELL INTERNATIONAL INC. EASA.IM.A.S.01671 FAA STC SA01253WI-D PILATUS PC-12/45 RVSM (FAA STC SA01253WI-D issue dated PC-12/45: MSN 101 to 835 (except MSN 20/02/2007) 545)PC-12/47: MSN 684 to 835 10015745 HONEYWELL INTERNATIONAL INC. EASA.IM.A.S.01776 FAA STC ST00491SE BOEING DC-9-81 (MD-81) FAA STC ST00491SE "Installation of the BOEING DC-9-82 (MD-82) BOEING DC-9-83 (MD-83) BOEING DC-9-87 (MD-87) BOEING MD-90-30 Enhanced Ground Proximity Warning System" 10015756 HONEYWELL INTERNATIONAL INC. EASA.IM.A.S.01790 ST01619SE BOEING 747-400 Introduction of Honeywell International Inc. Main/Nose Wheel pn. 2615901-1 and Carbon Brake pn. 2615902-1 in accordance with Honeywell Service Bulletin 2615901-32- 001_2615902-32-001 Revision New or later FAA-approved revision as replacement for Goodrich Br 10015805 HONEYWELL INTERNATIONAL INC. EASA.IM.A.S.01870 FAA STC ST00705SE BOEING 747-100 Installation of Honeywell Enhanced Ground BOEING 747-100F BOEING 747-300 BOEING 747-SP Proximity Warning System (EGPWS). 10015806 HONEYWELL INTERNATIONAL INC. EASA.IM.A.S.01871 FAA STC ST00140AT AIRBUS A310-200 Installation of MUA-45 Data Link System in AIRBUS A310-300 Airbus A310-200 / -300 series aircraft. 04/01/2013 Page 273/462 02.06.2008 29.01.2007 10.01.2005 31.03.2008 02.04.2009 30.06.2006 29.06.2005 17.08.2005 28.11.2005 02.05.2006 15.05.2007 15.05.2007 05.03.2007 22.03.2006 06.09.2007 12.04.2007
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