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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 10040972 TIMCO AEROSYSTEMS FAA STC NO. ST03928AT-D 777-300 Audio/Video On-Demand & In-seat Power none JADE/JAMCO STC ST02107SE-D must 10.08.2012 System Installation. be installed to or concurrently withthis STC.Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair 10015495 TIMCO AVIATION SERVICES INC. EASA.IM.A.S.01257 REV. 1 FAA STC ST03068AT-D BOEING 767-300 Cabin Standardization in accordance with This approval should not be extended to other 01.12.2006 TIMCO Master Data List 03T012L001, revision aircraft of this model on which other previoulsy D, dated November 30th, 2006, or later FAA approved modifications are incorporated approved revision. unless it is determined by the installer that the interrelationship between this change and any of those other previously 10015545 TIMCO AVIATION SERVICES INC. EASA.IM.A.S.01433 FAA STC ST03197AT BOEING 737-800 Complete interior reconfiguration in accordance 1. Compatibility of this design change with with TIMCO Aviation Services, Inc MDL, report other previously approved modifications must 17.07.2006 04T101L001, revision "C", dated December be determined by the installer.2. This STC is 07, 2005, or later EASA approved revision approved only for the product configuration as defined in the approved design data referred to in the paragraph "De 10015601 TIMCO AVIATION SERVICES INC. EASA.IM.A.S.01537 FAA STC ST03107AT-D BOEING 767-300 Interior Reconfiguration 15.12.2005 10015636 TIMCO AVIATION SERVICES INC. EASA.IM.A.S.01592 FAA STC ST01929AT-D BOMBARDIER DHC-8-100 SERIES BOMBARDIER DHC-8-200 SERIES BOMBARDIER DHC-8-300 SERIES Installation of Flight Data Recorder Expanded Parameters with a Plessey FDAU Limited to: 99T037C002 for DHC-8- 100/20000T029C009 for DHC-8- 300Maintenance required: pitch, roll and yaw position transducers and strings have to be detailed visually inspected and checked for smooth operation acc. MRB interval 2C 10015637 TIMCO AVIATION SERVICES INC. EASA.IM.A.S.01593 FAA STC ST03135AT-D BOEING 767-300 Installation of Rockwell Collins ACARS CMU- 900 28.11.2005 10015831 TIMCO AVIATION SERVICES INC. EASA.IM.A.S.01922 REV 1 FAA STC ST03372AT BOEING 767-300 Installation of Lower Lobe Crew Rest Module 1. This approval should not be extended to 16.01.2008 (CRM) and Main DeckVestibule in in other Aircraft of this model on which other accordance with Timco Master data List previously approved modifications are 04T104L001, Rev H, dated December 7, 2007 incorporated unless it is determined by the or later approved revisions approved by EASA installer that the interrelationship between this in accordance with EASA ED Decision 2004/04/CF (or change and any other previously ap 10015910 TIMCO AVIATION SERVICES INC. EASA.IM.A.S.02037 FAA STC ST03107AT-D BOEING 767-300 Interior Reconfiguration 16.08.2006 10015974 TIMCO AVIATION SERVICES INC. EASA.IM.A.S.02125 FAA STC ST03300AT-D AIRBUS A321 Installation of a doghouse (storage container) in Limitations and Conditions specified in FAA 18.01.2007 the bulk cargo compartment. STC ST03300AT-D remain applicable. 10015998 TIMCO AVIATION SERVICES INC. EASA.IM.A.S.02155 FAA STC ST03342AT-D BOEING DC-9-87 (MD-87) Installation of a Door Safety Strap 1. TIMCO’s Instructions For Continued 24.10.2006 BOEING MD-88 Airworthiness 06T005R014, Rev. IR dated June 8, 2006, is a required part of this STC.2. This STC is approved only for the product configuration as defined in the approved design data referred to in the paragraph 10016002 TIMCO AVIATION SERVICES INC. EASA.IM.A.S.02163 FAA STC ST01216AT-D AIRBUS A300 Installation of Airshow 210 System -- 08.10.2006 10027196 TIMCO AVIATION SERVICES INC. FAA STC ST00696AT-D B747-400 Installation of Collins SAT-906 SatCom System None Prior to installation of this modification it 14.09.2009 with Ball Antenna's inaccordance with Timco must be determined thatthe Master Data List MDL-01068, Revision M, interrelationship between this modification datedOctober 27, 1999 or later approved and any other previouslyinstalled revision. modification and/ or repair will introduce no adverse effectupon the airworthiness of the product. 10030407 TIMCO AVIATION SERVICES INC. FAA STC ST03820AT-D B767-300 Interior reconfiguration, B767-300Validation of FAA STC ST03820AT-D The aircraft will have the seating configuration changed to addadditional coach (Y) class seating, additional seat track installationwith associated structural modifications, removal of a 10014179 TMC AERO EASA.A.S.01316 AIRBUS A330-243 This STC deals with the installation of a TMC The approval of this modification is limited to stretcher. All documents related to this STC are the Airbus A330-243. the lmitations and listed in the STC form A330-25-23. The conditions defined in the EASA Datasheet are associated "Fiche de Modification" from Corsair is referenced 25-137 Rev. 1 ( or later EASA-approved revision ) applicable. 19.07.2006 As per FAA STC ST03820AT-D 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. 15.06.2010 04/01/2013 Page 450/462 02.06.2005
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10014180 TMC AERO EASA.A.S.01317 BOEING 737-400 Temporary Installation of a Stretcher that is 1. Operation of the aircraft with stretcher 29.08.2005 fitted on the Passengers Seat Track installed is limited to 100 FH per year2. The limitations as descrabied in the AFM Supplement Doc Ref AFMS25-0317 apply 10014181 TMC AERO EASA.A.S.01318 BOEING 747 The installation of stretchers mounted on the 1. The maximum number of passengers 12.07.2005 seat tracks in passenger cabin of the Boeing allowed when two stretchers are installed shall 747 for the transport of patients, as described be determined.2. When three or more in Corsair Fiche de Modification no. 25-136 stretchers are installed transport of passengers is not allowed. 10033808 TOST GMBH FLUGZEUGGERAETEBAU EASA.A.S.03948 LBA STC 0326/XXX HUSKY A-1A, A1-B Installation of Tow Cable retractor Winch with None Prior to installation of this modification it 23.06.2009 Guillotine to Husky A-1A,A-1B. Extension of must be determined thatthe LBA STC 0326/xxx, dated 21 October 1992. interrelationship between this modification This STC is a revision to and supersedes LBA and any other previouslyinstalled STC 0326/xxx, dated 21October 1992. modification and/ or repair will introduce no adverse effectupon the airworthiness of the product. The in 10028946 TQAS - TOTAL QUALITY AND AIRCRAFT B737-500 Installation of Floor proximity emergency photo luminescent path. 10031790 TQAS - TOTAL QUALITY AND AIRCRAFT A310-304 Cabin Modification to Full EconomyCabin Reconfiguration from a 18C/184Y seats configuration to a 224Yseats configuration 10014421 TRANSAIRCO S.A. EASA.A.S.01742 FOCA STC 23-15-001 ISS2 PILATUS PC-12 PILATUS PC-12/45 PILATUS PC-12/47 10014671 TRANSAIRCO S.A. EASA.A.S.02831 PILATUS PC-12 PILATUS PC-12/45 PILATUS PC-12/47 10014751 TRANSAIRCO S.A. EASA.A.S.02936 MYSTERE FALCON 900 MODE S TRANSPONDER WITH ENHANCED SURVEILLANCE CAPACITY 10014789 TRANSAIRCO S.A. EASA.A.S.02990 FOCA STC 31-31-05 FAN JET FAN JET FALCON SERIES C,D,E,F MYSTERE FALCON 20 C5, D5, E5 MYSTERE FALCON 20 F5 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. 22.02.2010 Limited to MSN 573 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 14.09.2010 Aircell 3100 Iridium SATCOM Installation 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. 07.09.2006 F.D.S.FD932 DVD Player Installation None 08.11.2006 AVIONICA mini QARAVIONICA mini QUAR P/NNote: This STC supersedes FOCA STC FOCA 31-31-05, dated 09.09.2002 10015474 TRANSAIRCO S.A. EASA.IM.A.S.01226 - MYSTERE FALCON 50 Replacement of existing HONEYWELL MK II GPWS and COLLINS MFD-85 with a UNIVERSAL Terrain Awareness and Warning system (TAWS) and a UNIVERSALMFD-640 This STC is approved only for those Mystere Falcon MF-900 aircraft excluding Falcon 900C version and incorporating at least:• Dual Collins TDR-94D Mode “S” ATC Transponders compliant with Elementary Surveillance and• Single or dual GPS receiver.Compa 1. Valid for Dassault Aviation:- Fan Jet Falcon Basic- Fan Jet Falcon Series C, D, E, F- Mystère-Falcon 20 Series C5, D5, E5, F52. This STC is approved only for the product configuration as defined in the approved design data referred to in the paragraphs 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 10015621 TRANSAIRCO S.A. EASA.IM.A.S.01573 - FALCON 20 Incorporation of Mode S EHS capability installer.2. Limited to F 1. Limited to Falcon 20 S/N 237; 257; 307; 341; 389; 4262. 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 sh 10015700 TRANSAIRCO S.A. EASA.IM.A.S.01688 - PC-12, PC-12/45 Structural installation of Honeywell KA-815 TCAS I Antennas 04/01/2013 Page 451/462 13.02.2007 23.01.2007 19.08.2005 14.09.2006 09.03.2006
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04/01/2013 Page 1/462 - EASA

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