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 10016123 FLYHT AEROSPACE SOLUTIONS Ltd. EASA.IM.A.S.02316 TCCA STC SA06-33 AIRBUS A319 AFIRS 220 Automated Flight Information ¿ AMS Instructions for Continued 20.07.2007 AIRBUS A320 Reportiing System Installationwith optional Airworthiness, Ref. 153-0029, Rev. A. AIRBUS A321 Global Voice and Global Text Satellite Compliance with the approved Airworthiness 10016213 FLYHT AEROSPACE SOLUTIONS Ltd. EASA.IM.A.S.02461 TCCA STC SA07-47 BOEING 757-200 Communication/EASA Validation of Transport Limitations contained therein is mandatory. Canada approved Supplemental TypeCertificate SA06-33. AFIRS 220 Automated Flight Information Reporting System Installation with Optional Gobal Voice and Global Text Satellite Communication. 13.09.2007 10016343 FLYHT AEROSPACE SOLUTIONS Ltd. EASA.IM.A.S.02659 TCCA STC SA07-7 BOMBARDIER DHC-8-100 Aeromechanical Services AFIRS (Automated 21.01.2008 SERIES Flight Information Reporting System) 220 BOMBARDIER DHC-8-200 installation with optional Global Voice and SERIES BOMBARDIER DHC-8-300 SERIES Global Text Satellite Communication. 10016344 FLYHT AEROSPACE SOLUTIONS Ltd. EASA.IM.A.S.02660 REV. 2 TCCA STC SA07-8 BOEING 737-200 SERIES AFIRS 220 Automated Flight Information Prior to installation of this modification the 22.05.2008 BOEING 737-300 SERIES Reporting System installation with Optional installer must determine that the BOEING 737-400 SERIES Global Voice and Global Text Satellite interrelationship between this modification and BOEING 737-500 SERIES Communication. any other previously installed modification will BOEING 737-600 SERIES introduce no adverse effect upon the BOEING 737-700 SERIES BOEING 737-800 SERIES airworthiness of the product. The install 10016385 FLYHT AEROSPACE SOLUTIONS Ltd. EASA.IM.A.S.02711 TCCA STC SA07-84 BOMBARDIER CL-600-2B19 AFIRS 220 Automated Flight Information AMS Instructions for Continued Airworthiness, 03.07.2008 (SERIES Reporting System installation with Optional Ref. 153-0036 Rev. A or later approved Global Voice and Global Text Satellite revision. Compliance with the approved Communication Airworthiness Limitations contained therein is mandatory. 10016522 FLYHT AEROSPACE SOLUTIONS Ltd. EASA.IM.A.S.02895 TCCA STC SA07-124 BOEING 767-200 AFIRS 220 Automated Flight Information Prior to installation of this modification the 19.08.2008 BOEING 767-300 Reporting System installation with Optional installer must determine that the Global Voice and Global Satellite interrelationship between this modification and Communication any other previously installed modification will introduce no adverse effect upon the airworthiness of the product.The installa 10027904 FLYHT AEROSPACE SOLUTIONS Ltd. EASA.IM.A.S.03184 REV. 4 TCCA STC SA08-7 HAWKER 750 HAWKER 800XP HAWKER 850XP HAWKER 900XP AFIRS 220 / AFIRS 228 Automated Flight Information Reporting SystemInstallation With Optional Global Voice and Global Text SatelliteCommunications. None. TCCA approved Airworthiness Limitations in Part I of AeroMechanicalServices Ltd ("FLYHT"), Instructions for Continued Airworthiness153-0040, Rev. D, dated 30 March 2011, or later TCCA accepted revisions,are mandatory for both the AFIRS 220 system and AFIRS 29.08.2012 10028338 FLYING COLOURS CORP. REV. 2 TCCA LSTC C-LSA09-326/D CL-600-2B19 Installation, Complete Custom Aircraft Interior Restricted to ASN 8092 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. 14.12.2011 10032278 FLYING COLOURS CORP. REV. 1 TCCA STC NO. SA10-66 CL-600-2B19 Installation, Equipment Bay Catwalk 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. 28.10.2010 10032279 FLYING COLOURS CORP. REV. 1 TCCA STC NO. SA10-67 CL-600-2B19 Installation, Equipment Bay Ladder Prior embodiment of EASA STC No. Prior to installation of this modification it 28.10.2010 10032278 'Installation, Equipment BayCatwalk' must be determined thatthe is required. 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 222/462
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10032280 FLYING COLOURS CORP. REV. 1 TCCA STC NO. SA10-65 CL-600-2B19 Installation, Equipment Bay Access Door Steps 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. 28.10.2010 10039852 FLYING COLOURS CORP. TCCA STC NO. SA12-33 CL-600-2B19 Installation, Aft Equipment Bay Tow Bar Stowage Provisions 10016455 FLYING INVESTMENTS, LLC EASA.IM.A.S.02801 FAA STC ST01349WI FAN JET FAN JET FALCON SERIES C FAN JET FALCON SERIES D FAN JET FALCON SERIES E FAN JET FALCON SERIES F FAN JET FALCON SERIES G MYSTERE FALCON 20-C5 MYSTERE FALCON 20-D5 MYSTERE FALCON 20-E5 MYSTERE FALCON 20-F5 10016456 FLYING INVESTMENTS, LLC EASA.IM.A.S.02802 FAA STC ST00571DE FAN JET FAN JET FALCON SERIES C FAN JET FALCON SERIES D FAN JET FALCON SERIES E FAN JET FALCON SERIES F FAN JET FALCON SERIES G MYSTERE FALCON 20-C5 MYSTERE FALCON 20-D5 MYSTERE FALCON 20-E5 MYSTERE FALCON 20-F5 10041003 FMD FLUGPLATZ MAGDEBURG EASA.A.S.03983 1. 172E,172F,172H,172K,172L 1. 172M,172N,172P,172R, 2. FR172E 10014607 FOKKER SERVICES B.V. EASA.A.S.02732 REV. 2 CL-600-2C10 (CRJ-700) VIP conversion of Bombardier CL600-2C10 (CRJ-700) for ConsolidatedContractors Company, as detailed in Fokker Services Reduced Vertical Separation Minimum (RVSM) Prior to installation of this modification the group airworthiness approval of specific installer must determine that the Dassault Aviation Fan Jet Falcon and Mystere- interrelationship between this modification and Falcon 20 aircraft in accordance with Flying any other previously installed modification will Investments LLC Master Drawing List introduce no adverse effect upon the MDL1017, Revision G, dated 19th February airworthiness of the product. The install 2008 Installation of an Innovative Solutions & Prior to installation of this modification the Supports (IS&S) Dual Air Data Display Units installer must determine that the (ADDU), an Analog Interface Unit or Air Data interrelationship between this modification and Sensor and Goodrich Dual Pitot-Static Probes, any other previously installed modification will in accordance with Flying Investments Master introduce no adverse effect upon the Data List GEN-031217-001, Revision airworthiness of the product. The install 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. 30.05.2012 The certificate shall remain valid unless otherwise surrendered orrevoked. If the utilisation of the VIP converted aircraft deviates from theassumed utilisation (e.g. flight hours or flight profile) supporting thescheduled Engineering ReportFS-N594. Description of the maintenance requirements as defined by modification.Revision 2: Wireless handsets in Bombardier, theoperator of the aircraft will the Aircell telephone installation in aCRJ-700 have to review the adequ 10014752 FOKKER SERVICES B.V. EASA.A.S.02937 REV. 2 A319CJ Changes to Airbus A319CJ in addition to the The activation of the Zonal VIP Conversion introduced byEASA STC Dryer/Humidification System is not part ofthis A.S.02937 as described in Fokker Services Major Change. The installation of the Zonal B.V. EngineeringReport A319-SAG-CRR-0002 Dryer/HumidificationSystem is certified, Issue 1. This STC has been revised to clarify however the correct use and functioning is the text in the Limitations andConditions. notcertified. Therefore the Zonal Dryer/Humidificatio 10031332 FOKKER SERVICES B.V. EASA.A.S.03317 A318-112 A318-112 VIP conversion, for description see 1. Refer to Chapter 2, Limitations of the AFM Chapter 1.1 of. ComplianceRecord Report A18- Supplement Airbus A318Model A318-112 MAK-CRR-0001 issue 5 d.d. 29-5-2009 Aircraft for the VIP Conversion As installed in Serialnumber 3238 issue 5 d.d. 29-5-20092. The STC is approved only for the product configuration as defined inthe approved d 10034242 FOKKER SERVICES B.V. P-EASA.A.S.03722 AIRBUS A320-232 Airbus A320-232 VIP Conversion. Refer to Limitations section of the approved AFM Supplement:A320-CAI-AFM-S- APPROVAL issue 1, dated 15th March 2011.Remarks: The aircraft type, model and manufacturer serial number forwhich this change is applicable is: Airbus A320-232 with ManufacturerSeri 22.07.2008 22.07.2008 This STC is a revision of and supersedes 29.07.2009 LBA STC SA1303, dated 15 April2003. Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair 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 21.01.2010 product. Prior to installation of this modification it 01.07.2010 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 the installer must determinethat the interrelationship between this modification and any otherpreviously installed modification will introduce no adverse effect uponthe airworthiness of the product. The installati 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. 04/01/2013 Page 223/462 29.05.2009 18.03.2011
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04/01/2013 Page 1/462 - EASA

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