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 10032538 ZF LUFTFAHRTTECHNIK GmbH REV. 2 MBB-BK 117 C-2 Main Gear Box Eurocopter BK117 - This conversion can only be performed by the Prior to installation of this modification it 13.06.2012 C2Conversion of the Main Gear Box from MBB- STC holder.- After conversion to Main Gear must be determined thatthe BK117 C-1 built standard PartNumber (P/N) Box P/N B632K1001-051 this is only to interrelationship between this modification 1171200501 to MBB-BK117 C-2 built standard beinstalled on MBB-BK117 C-2 helicopters. and any other previouslyinstalled P/NB632K1001-051 within the scope of a modification and/ or repair will introduce major overhaul, as documented in theZF no adverse effectupon the airworthiness Luftfahrttechnik (Z of the product 10031018 ZIM FLUGSITZ GmbH A310-300 Replacement of E/C seats by ZIM E/C seats, Type ECO-01This STC consists in replacing the existing seats by Type ECO-01seat. 10042845 ZIM FLUGSITZ GmbH REV. 1 B737-800 Installation of ZIM Flugsitz ECO-01 EC Seats in 1) The In-Seat IFE system shall not be used a B737-800 Cabin during Taxi, Take-Off andLanding.2) The ZIM Flugsitz ECO-01 EC Seats installation in accordance with thisSTC islimited to the following B737-800 aircraft S/N 41047 and 41190. 10013965 ZOREX AIR TRANSPORT EASA.A.S.00659 REV. 1 FAIRCHILD SWEARINGEN SA 226-TC COMM/NAV/GPS Garmin GNS430 Installation, for B-RNAV Operation, and COMM Bendix King KY196A Installation, both for 8.33 kHz standard. 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. 21.07.2010 1. The aircraft is approved for dual pilot B- RNAV operation, subjected to the conditions, limitations and procedures contained in: . Anexo 8 al Programa de Certificación "Aircraft Flight Manual Supplement", Ed. inicial.2. This STC is approved only fo Prior to installation of this STC it must be determined that theinterrelationship between this STC and any other previously installedmodification and / or repair will introduce no adverse effect upon theairworthiness of the product. 04/01/2013 Page 462/462 21.12.2012 25.04.2006
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04/01/2013 Page 1/462 - EASA

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