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 />
10038864 BOMBARDIER INC. TCCA STC SA11-96 BD-700-1A10 Installation of a Frequency Converter Fuse 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 />
20.03.2<strong>01</strong>2<br />
10039764 BOMBARDIER INC. TCCA STC SA12-16, ISSUE 2 BD-700-1A10 Installation, Aircraft Completion Modifications -<br />
ASN 9440.<br />
10039790 BOMBARDIER INC. TCCA STC Q-LSA00-009/D ISSUE 1 BD-700-1A10 Transport Canada STC No. Q-LSA00-009/D -<br />
Installation of Interior andAvionics.<br />
Restricted to ASN 9440.The Wireless Local<br />
Area Network (WLAN) is intended to provide<br />
internetconnectivity and email services to the<br />
airplane's cabin using portableelectronic<br />
devices (PEDs). Any other intended function of<br />
this equipmentwill require a re-ex<br />
Restricted to ASN 9028.Installation of <strong>EASA</strong><br />
STC No. 10039791 is a pre-requisite.<br />
10039791 BOMBARDIER INC. TCCA STC C-LSA12-<strong>04</strong>0/D ISSUE 1 BD-700-1A10 Installation, Modifications to Interior Completion Restricted to ASN 9028. Installation of <strong>EASA</strong><br />
- ASN 9028.<br />
STC No. 10039790 is apre-requisite.<br />
10039792 BOMBARDIER INC. TCCA STC LSA<strong>01</strong>-329 ISSUE 2 BD-700-1A10 Approval of Seating Limitations for Center &<br />
Aft Positions of Aft RHSDivan (FS 663).<br />
10039808 BOMBARDIER INC. TCCA STC SA12-16, ISSUE 2 BD-700-1A11 Installation, Aircraft Completion Modifications -<br />
ASN 9453<br />
10<strong>04</strong><strong>01</strong>71 BOMBARDIER INC. TCCA STC NO. SA12-16 BD-700-1A10 Installation, Aircraft Completion Modifications -<br />
ASN 9450<br />
10<strong>04</strong><strong>01</strong>72 BOMBARDIER INC. TCCA STC NO. SA12-16 BD-700-1A10 Installation, Aircraft Completion Modification -<br />
ASN 9441<br />
10<strong>04</strong>0256 BOMBARDIER INC. TCCA STC NO. SA12-16 BD-700-1A10 Installation, Aircraft Completion Modifications -<br />
ASN 9455.<br />
Prior to installation of this modification it 22.05.2<strong>01</strong>2<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 />
Prior to installation of this modification it 23.05.2<strong>01</strong>2<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 />
Prior to installation of this modification it 23.05.2<strong>01</strong>2<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 />
Restricted to ASN 9028.Previous installation of Prior to installation of this modification it<br />
<strong>EASA</strong> STC No. 10039790 and <strong>EASA</strong> STC No. must be determined thatthe<br />
23.05.2<strong>01</strong>2<br />
10039791are pre-requisites.The aircraft is interrelationship between this modification<br />
limited to private use only, unless the<br />
and any other previouslyinstalled<br />
conditionsspecified in Flight Manual<br />
modification and/ or repair will introduce<br />
Supplement D00691 Revision N/C are no adverse effectupon the airworthiness<br />
satisfied.<br />
of the product.<br />
Restricted to ASN 9453.The Wireless Local<br />
Area Network (WLAN) is intended to provide<br />
internetconnectivity and email services to the<br />
airplane's cabin using portableelectronic<br />
devices (PEDs). Any other intended function of<br />
this equipmentwill require a re-exa<br />
Restricted to ASN 9450The Wireless Local<br />
Area Network (WLAN) is intended to provide<br />
internetconnectivity and email services to the<br />
airplane's cabin using portableelectronic<br />
devices (PEDs). Any other intended function of<br />
this equipmentwill require a re-exam<br />
Prior to installation of this modification it 24.05.2<strong>01</strong>2<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 />
Prior to installation of this modification it 15.06.2<strong>01</strong>2<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 />
Restricted to ASN 9441.The Wireless Local Prior to installation of this modification it 15.06.2<strong>01</strong>2<br />
Area Network (WLAN) is intended to provide must be determined thatthe<br />
internetconnectivity and email services to the interrelationship between this modification<br />
airplane's cabin using portableelectronic and any other previouslyinstalled<br />
devices (PEDs). Any other intended function of modification and/ or repair will introduce<br />
this equipmentwill require a re-exa<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
Restricted to ASN 9455.The Wireless Local<br />
Area Network (WLAN) is intended to provide<br />
internetconnectivity and email services to the<br />
airplane's cabin using portableelectronic<br />
devices (PEDs). Any other intended function of<br />
this equipmentwill require a re-exa<br />
Prior to installation of this modification it 21.06.2<strong>01</strong>2<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 />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 137/<strong>462</strong>
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