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 10014814 STC TWENTY ONE LIMITED EASA.A.S.03022 REV 2 BOMBARDIER CL-600-2B19 Introduction of Passenger Cabin interior. EASA STC No. EASA.IM.A.S.01752 must be fitted.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 16.01.2009 10014900 STC TWENTY ONE LIMITED EASA.A.S.03130 737- 600, 700, 800, 900 Installation of Cabin Vu-123 Cabin Surveillance 737-200, 300, 400, 500, System. 10014918 STC TWENTY ONE LIMITED EASA.A.S.03164 BOMBARDIER CL-600-2B16 (604) Introduction of Passenger Cabin Interior. 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. The install 10014997 STC TWENTY ONE LIMITED EASA.A.S.03297 REV 1 BOEING 767-200 BOEING 767-300 10015018 STC TWENTY ONE LIMITED EASA.A.S.03324 CESSNA 500, CITATION CESSNA 550 10015068 STC TWENTY ONE LIMITED EASA.A.S.03394 AIRBUS A318 AIRBUS A319 AIRBUS A320 AIRBUS A321 23.01.2008 25.08.2008 Introduction of CabinVu-123 Cabin Surveillance System 20.05.2008 Introduction of Dual GNS-430/530 05.05.2008 Introduction of Wingspeed XLLink Communications and Data Management 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. The install 10015109 STC TWENTY ONE LIMITED EASA.A.S.03452 BOMBARDIER CL-600-2B19 Introduction of Passenger Cabin interior. 07.03.2008 10015115 STC TWENTY ONE LIMITED EASA.A.S.03464 SAAB SF340A Rework of Class E cargo role of QC variant 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. The install 19.12.2008 10015176 STC TWENTY ONE LIMITED EASA.A.S.03553 BOEING 737-300 Carriage of Horses & Grooms 1. This design change is applicable to Boeing 737-300 aircraft converted under FAA STC SA2968SO, SA2969SO, and SA2970SO & SA2971SO as previously been validated by the UK CAA under Airworthiness Approval Note AAN 24984.2. The certification basis has b 10015185 STC TWENTY ONE LIMITED EASA.A.S.03568 BOMBARDIER BD-700-1A11 Introduction of Passenger Cabin Interior. 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. The i 23.12.2008 10015199 STC TWENTY ONE LIMITED EASA.A.S.03590 BOEING 767-200 Introduction of Change 7.0 ACAS II and Dual Mode S 12.06.2008 10017185 STC TWENTY ONE LIMITED EASA.R.S.01318 AS 355 F1 Introduction of Skylark 2 Radar. 01.02.2007 10017212 STC TWENTY ONE LIMITED EASA.R.S.01368 R44 R44 II Installation of removable crop spraying equipment onto Robinson R 44 & R 44 II helicopters 1. Certified in Restricted Category2. All limitation of RFM supplement apply3. Prior to installation of this modification the installer must determine that the interrelationship between this modification and any other previously installed modifica 10026853 STC TWENTY ONE LIMITED P-EASA.A.S.03708 REV. 1 BOMBARDIER CL-600-2B19 Introduction of Wireless Local Area Network. 1. Prior to installation of this modification 20.08.2009 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 insta 10028521 STC TWENTY ONE LIMITED BD-700-1A10 Customized Aircraft Completion - ASN 9251. 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. 19.01.2010 04/01/2013 Page 422/462 29.10.2008 07.04.2009 01.08.2007
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10029416 STC TWENTY ONE LIMITED P-EASA.A.S.03895 BD-700-1A10 Customized Aircraft Completion - ASN 9266 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. 24.03.2010 10030161 STC TWENTY ONE LIMITED 1. CESSNA 337 2. REIMS CESSNA 337 Introduction of Bubble Windows Restricted to un-pressurized versions of the Cessna/Cessna Reims 337aircraft 10030229 STC TWENTY ONE LIMITED P-EASA.A.S.03972 B757-200/ -300 Introduction of Air Conditioning Filter Installation of STC21 Limited Minor Change S21.21-15-1004, must beembodied prior to, or concurrent with, this STC 10030237 STC TWENTY ONE LIMITED P-EASA.A.S.03926 SAAB SF340A, SAAB 340B Rework of the Class E Compartment for inclusion of a courier seatingarea for up to 5 occupants, S21.25-63-1355. 10030991 STC TWENTY ONE LIMITED REV. 1 L-410 UVP-E20 CARGO L-410 UVP-E9 L-410 UVP, L-410 UVP-E, 10031459 STC TWENTY ONE LIMITED F 406 Installation of Thales I-MASTER A-Flight Radar Turret EASA.A.S.01681 R1 and EASA.A.S.01738 must be installed Prior to installation of this modification it 31.05.2010 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 it 04.06.2010 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 it 04.06.2010 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 Introduction of under wing emergency exits. None None 11.06.2012 10031662 STC TWENTY ONE LIMITED CL-600-2B16 Introduction of Swift Broadband 1. The Airworthiness Approval of the wireless system does not constituteOperational Approval for the use of transmitting PEDs on 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. 17.08.2010 Prior to installation of this modification it must be determined thatthe interrelationship between this modification board of theaircraft. Operational Approval must and any other previouslyinstalled be obtained from the responsibledivision of the modification and/ or repair will introduce operational authority of the ai no adverse effectupon the airworthiness of the product. 10031863 STC TWENTY ONE LIMITED B757-200 Introduction of CabinVu-123 Cabin Surveillance None Prior to installation of this modification it 20.09.2010 System 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 10031961 STC TWENTY ONE LIMITED BD-700-1A10 Customized Aircraft Completion - ASN 9365 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. 27.09.2010 04/01/2013 Page 423/462 02.09.2010
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04/01/2013 Page 1/462 - EASA

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