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 />
10<strong>01</strong>4464 BINDER MOTORENBAU GmbH <strong>EASA</strong>.A.S.02525 ALEXANDER SCHLEICHER ASH Modification of outer wing panel with winglets<br />
02.03.2006<br />
25 E<br />
and 27 m wingspan<br />
10<strong>01</strong>4471 BINDER MOTORENBAU GmbH <strong>EASA</strong>.A.S.02532 ALEXANDER SCHLEICHER ASW Binder Motorenbau Technische Mitteilung ASW This STC is approved only for the product<br />
12.<strong>04</strong>.2006<br />
22 BL<br />
22 BLE B2Changes in engine installation:- configuration as defined in the approved design<br />
Different type of spindle drive- Installation of a data referred to in the paragraph "Description".<br />
primer ball- CFRP gear mount<br />
Compatibility with other aircraft/engine<br />
configurations shall be determined by the<br />
installer.<br />
10<strong>01</strong>4490 BINDER MOTORENBAU GmbH <strong>EASA</strong>.A.S.02552 ALEXANDER SCHLEICHER ASH Modification of outer wing panel with winglets<br />
03.02.2006<br />
25<br />
and 27 m wingspan<br />
10029418 BINDER MOTORENBAU GmbH P-<strong>EASA</strong>.A.S.03569 NIMBUS-3DM Nimbus-3DM - Umbau von Rotax535C auf None. Prior to installation of this modification the 24.03.2<strong>01</strong>0<br />
Solo 2625/2<br />
installer must determinethat the<br />
interrelationship between this modification<br />
and any otherpreviously installed<br />
modification will introduce no adverse<br />
effect uponthe airworthiness of the<br />
product.The approval ho<br />
10034252 BINDER MOTORENBAU GmbH ASH 25 E Conversion from hand starter to electric<br />
starter.Umbau Handstarter auf Elektrostarter.<br />
None. None. 21.03.2<strong>01</strong>1<br />
10036110 BINDER MOTORENBAU GmbH ETA None. None. 11.08.2<strong>01</strong>1<br />
10<strong>04</strong>2442 BINDER MOTORENBAU GmbH DG-500 M DG500M - Umbau von Rotax535C auf Solo<br />
2625/2<br />
None. None. 30.11.2<strong>01</strong>2<br />
10028420 BIZJET INTERNATIONAL REV. 1 FAA STC ST10964SC A318-112 Installation of provisions for an Executive Not applicable Prior to installation of this modification it 14.10.2<strong>01</strong>0<br />
Power System<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 />
10028421 BIZJET INTERNATIONAL REV. 1 FAA STC ST10963SC A318-112 Installation of a Miltope Wireless Access Point Not applicable 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 />
14.10.2<strong>01</strong>0<br />
10028425 BIZJET INTERNATIONAL REV. 8 FAA STC ST10958SC A318-112, A319-133 Installation of a Cabin VIP InteriorMajor<br />
Change to the <strong>EASA</strong> STC 10028425 REV 7<br />
introducing changes in theCabin VIP Interior<br />
Installation (add the -007 configuration)<br />
10<strong>04</strong>2292 BIZJET INTERNATIONAL SALES AND<br />
SUPP<br />
10<strong>01</strong>6472 BJAC BUSINESS JET AIRCRAFT <strong>EASA</strong>.IM.A.S.02818 TC STC SA07-129 ISSUE 1 BOMBARDIER BD-700-1A10<br />
BOMBARDIER BD-700-1A11<br />
10<strong>01</strong>5400 BLACKHAWK MODIFICATIONS Inc. <strong>EASA</strong>.IM.A.S.<strong>01</strong>110 FAA STC SA10341SC BEECH C90<br />
BEECH C90A<br />
BEECH E90<br />
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 />
31.07.2<strong>01</strong>2<br />
FAA STC ST09033SC MYSTERE FALCON 50 Installation of a quick drain kit on Environmental None Prior to installation of this modification it 21.11.2<strong>01</strong>2<br />
Control UnitValidation of FAA STC<br />
must be determined thatthe<br />
ST09033SC<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 />
Goodrich Class III Electronic Flight Bag. Prior to installation of this modification the<br />
installer must determine that the<br />
interrelationship between this modification and<br />
any other previously installed modification will<br />
introduce no adverse effect upon the<br />
airworthiness of the product. The install<br />
Installation of Pratt & Whitney Canada PT6A- 1. AFMS No 19005, Rev IR 24 November<br />
135A (de-rated to 550 HP) engines and 20<strong>04</strong> oe later approved revision is required for<br />
McCauley 4HFR34C762/94LMA-4 or the Raytheon C90, C90A or E90 airplane with<br />
4HFR34C768/94LMA-4propellers in<br />
Pratt& Whitney Canada PT6A-135A engines.<br />
accordance with Blackhawk Modifications Inc Note that the Horsepower is limited to 550 at<br />
Drawing No 19005-<strong>01</strong> Rev IR, dated 15 March 1900 RPM.2. Each engine mount must be re<br />
20<strong>04</strong>, "Installation Inst<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 114/<strong>462</strong><br />
14.10.2008<br />
29.03.2006
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