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 10029250 AERO TECHNICS DESIGN LIMITED A300, A310 Introduction of Instone Airservices Airstable This STC is approved only for the product None. 26.03.2010 B747-400, DC-8, DC-10.MD-11, Horse/Freight ContainerP/N 73-90-343. configuration as defined inthe approved design B767, L100/L1011, B777 data referred to in the paragraph ’Description’. Compatibility with all aircraft configurations shall be determined bythe installer. 10031612 AERO TECHNICS DESIGN LIMITED B737-500 Cabin Seating Reconfiguration from 120Y to 16C/28C layout (44C) 10031614 AERO TWIN, Inc. FAA STC SA4625NM CESSNA 208, 208B Fabrication and Installation of Aero Twin, Inc EB8-200 extended baggagekit in accordance to FAA STC SA4625NM 10033295 AERO TWIN, Inc. P- EASA.IM.A.S.02690 FAA STC SA02291AK CESSNA 208, 208B Installation of Honeywell TPE331-12JR turbine engine and HartzellHC-B4TN- 5QL/LT10890N(K) propeller and associated structure and equipmentin accordance with FAA STC SA02291AK. 10037001 AERO TWIN, Inc. FAA STC SA4626NM CESSNA 208, 208B Fabrication and Installation of Auxiliary dry air pump kit AP8-100 inaccordance to FAA STC SA4626NM. 10038365 AERO TWIN, Inc. FAA STC SA02080AK-D 208, 208B Fabrication and Installation of Aero Twin, Inc. Exhaust Deflector P/NED8-100 in accordance with FAA STC SA02080AK-D 10027700 AERO VODOCHODY A.S. P-EASA.A.S.03909 REV. 1 EMB-135BJ EFB class2 navAero- t.BagC2² Electronic Bag System implementation 10037255 AERO VODOCHODY A.S. REV. 1 A330-201, -202, -203 A330-223, -223F A330-243, -243F A330-301, -302, -303 A330-321, -322, -323 A330-341, -342, -343 Implementation of Electronic Flight Bag Class 2This STC installs provisions for Class 2 EFB (navAero T.Bag C²). 10040961 AERO VODOCHODY A.S. REV. 1 A300 SERIES, A310 SERIES Implementation of provisions for EFB Class2, NavAero T.Bag C2 inaccordance with Aero Vodochody MDL AM003-MDL Rev 4. Rev 1 of this STC addresses the installation of power switches to the28V DC bus for safe power off for the EFB-system. Limited to B737-500 S/N 24645, 24648 and 24649 Prior to installation of this modification it 31.08.2010 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. 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. 31.08.2010 a) This modification is not compatible withi. Cessna 208 serial numbers 20800001 through 20800013, 20800416,20800500 and greaterii. Cessna 208B serial numbers 208B1190, 208B1216, 208B2000 and greateriii. FAA STC SA01478WIb) This modification has been verif 1. The following modifications are 12.01.2011 required for Cessna 208 (208A) aspart of this modification:a) Wipaire Inc.; Installation of Vortex Generator in combination withGross Weight Increase, FAA STC SA270CHb) Aero Twin, Inc., Auxiliary Vacuum Pump, FAA STC SA46 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. 24.10.2011 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 09.02.2012 -Application of Electronic Checklist/ECL and WLAN need a separateapproval-No external devises are approved to be connected to the display duringmovement/flight of the aircraft. EMB-135 model BJ not affected by EWIS requirements 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 20.07.2010 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 29.11.2011 FOR MSN 0554, 0560; 0614 AND 0667, REVISION 1 OF THIS RAPPROVAL IS VALIDONLY UNDER THE FOLLOWING CONDITION: ACCOMPLISHMENT OF INSTALLATION OFSWITCHES ACCORDING TO AERO VODOCHODY MINOR CHANGE, A-STC-Z 0058 FOR MSN0554, A-STC-Z 0059 FOR MSN 0560, A-STC-Z 006 Prior to installation of this modification it 31.10.2012 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. 04/01/2013 Page 14/462
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10029795 AEROACOUSTICS AIRCRAFT FAA STC SA02042SE CESSNA 208 Aircraft Payload Extender (APE) STOL System Note 1: This modification is also applicable to Prior to installation of this modification it 21.04.2010 SYSTEMS, INC for Cessna 208 and 208A inacc. to FAA STC the following aircraft that have been modified must be determined thatthe SA02042SE with Wipaire, Inc. STC No. SA149CH (675 interrelationship between this modification SHP PT6A-114A Engine Installation). and any other previouslyinstalled Model,,Serial Number,,,,,,Note 208,,,,2080001 modification and/ or repair will introduce through 20800060,,Eligible only if mo no adverse effectupon the airworthiness of the product. 10029821 AEROACOUSTICS AIRCRAFT SYSTEMS, INC 10033826 AEROACOUSTICS AIRCRAFT SYSTEMS, INC 10033827 AEROACOUSTICS AIRCRAFT SYSTEMS, INC 10016152 AEROCET, INC. EASA.IM.A.S.02354 FAA STC SA00137SE CESSNA 180A CESSNA 180H CESSNA 180J CESSNA 180K FAA STC SA01805SE 208B Aircraft Payload Extender (APE) STOL System The installation must be maintained in in acc. to FAA STC SA01805SE accordance with Section 3.0 ofDocument No. AA1976 FAA STC SA01239SE 208 Fabrication and installation of AeroAcoustics Aircraft Systems (AAIS)Aircraft Payload Extender III (APE III) system in acc. with FAA STCSA01239SE. FAA STC SA01180SE 208 Fabrication and installation of AeroAcoustics Aircraft Systems (AAIS)Aircraft Payload Extender II (APE II) system in acc. with FAA STCSA01180SE. 10016153 AEROCET, INC. EASA.IM.A.S.02355 FAA STC SA5908NM CESSNA 185A CESSNA 185B CESSNA 185C CESSNA 185D CESSNA 185E CESSNA A185E CESSNA A185F 10016154 AEROCET, INC. EASA.IM.A.S.02356 FAA STC SA00003SE CESSNA P206 CESSNA P206A CESSNA TP206A CESSNA TU206A CESSNA TU206B CESSNA TU206C CESSNA TU206D CESSNA TU206E CESSNA TU206F CESSNA TU206G CESSNA U206A CESSNA U206B CESSNA U206C CESSNA U206D CESSNA U206E CESSNA U206F CESSNA U206G 10015746 AEROCON ENGINEERING COMPANY EASA.IM.A.S.01778 FAA STC ST01086LA JETSREAM 4100 Installation of Smoke Detection & Fire Suppression Systems for Conversion of Class D Cargo Compartments to Class C 10014554 AEROCONDOR TRANSPORTES AEREOS SGPS 10014754 AEROCONDOR TRANSPORTES AEREOS SGPS Prior to installation of this modification it 22.04.2010 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 This modification is limited to the following If the STC holder agrees to permit 10.02.2011 landplanes (serialnumbers) only: 20800001 another person to use thiscertificate to through 20800060 (eligible only if modified with alter the product, the STC holder shall Cessna KitSK-208-12) 20800061 and up give the otherperson written evidence on Speed limits: Maneuvering Speed @ 8.362 lbs: that permission.Prior to installation of this 143 KIASCG Range: Takeoff and Flight modification it must be determined thatthe interrelat Additional limitation: Refer to original FAA STC If the STC holder agrees to permit SA01180SESerial Number:20800001 through another person to use thiscertificate to 20800060 (eligible only if modified with Cessna alter the product, the STC holder shall 10.02.2011 KitSK-208-12)20800061 and upThis give the otherperson written evidence on modification is also applicable to the following that permission.Prior to installation of this aircraft equippedwith Wipline Model 8 modification it must be determined thatthe interrelat Installation of Aerocet Model 3500 or 3500L Those Cessna Model 180G, 180H, 180J and 09.08.2007 seaplane floats on Cessna 180 Aircraft. 180Kairplanes equipped with the structural modifications defined in Kenmore Air Harbour STCNo. SA649NW, Amendment dated 14 July 1984, may be operated on Aerocet Model 3500 or 3500L floats at gross weight up to 3190lb Installation of Aerocet Model 3500 or 3500L The airplane must incorporate the Cessna 09.08.2007 seaplane floats on Cessna 185 Aircraft. approved seaplane kit referred to Section 7 of the Aerocet AFM. The airplane must be equipped with the Cessna rudder centering device/non-linear rudder centering spring system defined on Aerocet Drawing No. 35- 10000 Installation of Aerocet Model 3500 or 3500L seaplane floats 03.07.2007 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 EASA.A.S.02652 DORNIER DO 228-202K Installation of Honeywell TCAS system CAS- 67A with Diversity Mode S Transponder MST- 67A, Control Unit PS-550 and two E-VSI IVA- 81A 21.11.2006 EASA.A.S.02940 Installation of TAWS As per AFM 26.03.2007 04/01/2013 Page 15/462 17.02.2006
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04/01/2013 Page 1/462 - EASA

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