04/01/2013 Page 1/462 - EASA
04/01/2013 Page 1/462 - EASA
04/01/2013 Page 1/462 - EASA
Create successful ePaper yourself
Turn your PDF publications into a flip-book with our unique Google optimized e-Paper software.
<strong>EASA</strong> STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue<br />
10028181 BOMBARDIER INC. TCCA STC SA05-60 BD-700-1A11 Installation, Complete Custom Aircraft Interior - Restricted to ASN 9231 Prior to installation of this modification it 07.12.2009<br />
ASN 9231<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 />
10028344 BOMBARDIER INC. BD-700-1A10 Installation, Complete Custom Aircraft Interior -<br />
ASN 9320<br />
10028416 BOMBARDIER INC. REV. 2 TCCA STC SA<strong>04</strong>-113 BD-700-1A10 Modification to install the Fwd Pocket door and<br />
Mid Pocket door on aseparate<br />
circuitInstallation, Complete Custom Aircraft<br />
Interior - Revision to <strong>EASA</strong>Supplemental Type<br />
Certificate 10028416 to incorporate missing<br />
drawingson the MDL - ASN 9329<br />
10028519 BOMBARDIER INC. TCCA STC NO. SA<strong>04</strong>-113 BD-700-1A10 Installation, Complete Custom Aircraft Interior -<br />
ASN 9333<br />
10028553 BOMBARDIER INC. TCCA STC NO. SA<strong>04</strong>-113 BD-700-1A10 Installation, Complete Custom Aircraft Interior -<br />
ASN 9115<br />
10028579 BOMBARDIER INC. REV. 2 TCCA STC SA05-60 BD-700-1A11 Installation, Interior Completions In-Service<br />
Improvement Modifications- ASN 9334<br />
10029275 BOMBARDIER INC. TCCA STC SA<strong>04</strong>-113 BD-700-1A10 Installation, Complete Custom Aircraft Interior -<br />
ASN 9323.<br />
10029589 BOMBARDIER INC. TCCA STC SA10-19 BD-700-1A10 Installation, Upgrade from Swift 63 to Swift<br />
Broadband<br />
10029628 BOMBARDIER INC. TCCA STC SA<strong>04</strong>-113 BD-700-1A10 Installation, Complete Custom Aircraft Interior -<br />
ASN 9336<br />
Restricted to ASN 9320 and1. Refer to the<br />
Limitations sections of the required AFM<br />
Supplement andto the referenced FCOMS.2.<br />
WLAN system is compatible only to IEEE<br />
802.11(b).3. Prior to installation of this<br />
modification the installer mustdetermine that<br />
the<br />
Restricted to ASN 9329 and1. Refer to the<br />
Limitations sections of the required AFM<br />
Supplement andto the referenced FCOMS.2.<br />
WLAN system is compatible only to IEEE<br />
802.11(b).<br />
Restricted to ASN 9333 and1.Refer to the<br />
Limitations sections of the required AFM<br />
Supplement andto the referenced<br />
FCOMS.2.WLAN system is compatible only to<br />
IEEE 802.11(b).<br />
Restricted to ASN 9115 and1.Refer to the<br />
Limitations sections of the required AFM<br />
Supplement andto the referenced<br />
FCOMS.2.WLAN system is compatible only to<br />
IEEE 802.11(b).<br />
Prior to installation of this modification it 18.12.2009<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 19.05.2<strong>01</strong>0<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 21.<strong>01</strong>.2<strong>01</strong>0<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 21.<strong>01</strong>.2<strong>01</strong>0<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 9334 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 />
08.08.2<strong>01</strong>1<br />
Restricted to ASN 9323.Refer to the<br />
Limitations sections of the required AFM<br />
Supplement and tothe referenced<br />
FCOMS.WLAN system is compatible only to<br />
IEEE 802.11(b).<br />
Prior to installation of this modification it 17.03.2<strong>01</strong>0<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 />
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 />
02.<strong>04</strong>.2<strong>01</strong>0<br />
Restricted to ASN 9336 and1. Refer to the<br />
Limitations sections of the required AFM<br />
Supplement andto the referenced FCOMS.2.<br />
WLAN system is compatible only to IEEE<br />
802.11(b).<br />
Prior to installation of this modification it 08.<strong>04</strong>.2<strong>01</strong>0<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> 130/<strong>462</strong>