04/01/2013 Page 1/462 - EASA
04/01/2013 Page 1/462 - EASA
04/01/2013 Page 1/462 - EASA
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<strong>EASA</strong> STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue<br />
10038140 LAZ-TEC, L.L.C. FAA STC SR00716DE BELL 429 Crew Door Assist Handle None Prior to installation of this modification it<br />
must be determined thatthe<br />
interrelationship between this modification<br />
and any other previouslyinstalled<br />
modification and/ or repair will introduce<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
23.<strong>01</strong>.2<strong>01</strong>2<br />
10<strong>01</strong>4950 LD AVIATION PRAGUE S.R.O. <strong>EASA</strong>.A.S.03213 CESSNA T303 COMM/NAV/GPS GNS 530, GNS 430,<br />
Navigation Indicator GI 106, S-mode GTX 330<br />
Transponder, GMA 340 ICS, and ELT Kannad<br />
406AF installation into Cessna T303.<br />
S/N: T303 00205. 15.11.2007<br />
10<strong>01</strong>4958 LD AVIATION PRAGUE S.R.O. <strong>EASA</strong>.A.S.03228 CESSNA T206H Installation of Leica RC30 with IPAS 10 and<br />
FCMS options.<br />
S/N T20608636. 19.10.2007<br />
10026761 LD AVIATION PRAGUE S.R.O. P-<strong>EASA</strong>.A.S.03837 CESSNA 172 RG Avionics Upgrade - GNS430W, KX165A, None. 1.,,Prior to installation of this modification 07.08.2009<br />
GMA340, GI106A, KN62A,<br />
the installer mustdetermine that the<br />
GTX330,KANNAD406AF Compact Installation<br />
interrelationship between this modification<br />
and anyother previously installed<br />
modification will introduce no adverse<br />
effectupon the airworthiness of the<br />
product.2.,,The ins<br />
10036826 LD AVIATION PRAGUE S.R.O. L 200A, L 200 D Avionics Upgrade , GNS 430W, GMA 347, WX None Prior to installation of this modification it 10.10.2<strong>01</strong>1<br />
500, KCS 55A , ELT 406, MID4200-10<br />
must be determined thatthe<br />
Installation<br />
interrelationship between this modification<br />
and any other previouslyinstalled<br />
modification and/ or repair will introduce<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
10029813 LE BOZEC FILTRATION & SYSTEMS<br />
SAS<br />
REV. 2 FAA STC ST09864SC 737-100, -200, -200C, -300<br />
737-400, -500<br />
Rain Repellent System Modification -<br />
Modification of Rain RepellentSystem in<br />
accordance with "Le Bozec, Inc.” documents.<br />
Only applicable to Rain repellent systems that Prior to installation of this modification it 06.08.2<strong>01</strong>2<br />
were installed at time ofairplane production must be determined thatthe<br />
under TC <strong>EASA</strong> IM.A.120 or FAA TC A16WE. interrelationship between this modification<br />
and any other previouslyinstalled<br />
modification and/ or repair will introduce<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
10031318 LEARJET INC FAA STC SA8119NM-D CL-600-2B16 Installation of the Bulkhead F.S.353 none Prior to installation of this modification it<br />
must be determined thatthe<br />
interrelationship between this modification<br />
and any other previouslyinstalled<br />
modification and/ or repair will introduce<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
10.08.2<strong>01</strong>0<br />
10031319 LEARJET INC FAA STC SA8120NM-D CL-600-2B16 Interior Installation - Main Cabin none Prior to installation of this modification it<br />
must be determined thatthe<br />
interrelationship between this modification<br />
and any other previouslyinstalled<br />
modification and/ or repair will introduce<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
10.08.2<strong>01</strong>0<br />
10031320 LEARJET INC FAA STC SA8122NM-D CL-600-2B16 Installation of the Armledge / Dado none Prior to installation of this modification it<br />
must be determined thatthe<br />
interrelationship between this modification<br />
and any other previouslyinstalled<br />
modification and/ or repair will introduce<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
10.08.2<strong>01</strong>0<br />
10<strong>01</strong>5312 LEARJET INC. <strong>EASA</strong>.IM.A.S.0<strong>01</strong>62 FAA STC ST<strong>01</strong>606LA-D BOMBARDIER BD-100-1A10<br />
(CHALLE<br />
The modification consists in the installation of 1. The Maintenance Instructions for<br />
an Executive Interior in accordance with Master Continued Airworthiness are contained in<br />
Drawing List HC20<strong>01</strong>350<strong>01</strong>, Rev. E dated July Documents Number HC20<strong>01</strong>35000-IFCA-1.<br />
10, 20<strong>04</strong> (or later FAA approved<br />
Modification of an aircraft by this STC obligates<br />
revision).Validation of FAA STC ST<strong>01</strong>606LA- the aircraft operator to include the maintenance<br />
D.<br />
information provided by this document in<br />
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07.10.20<strong>04</strong>
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