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 />
10030620 BOMBARDIER AEROSPACE BD-100-1A10 (CHALLENGER Installation of Miniature Quick Access Recorder None Prior to installation of this modification it 28.06.2<strong>01</strong>0<br />
300)<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 />
10030934 BOMBARDIER AEROSPACE REV. 1 TCCA STC SA10-50 BD100-1A10 Activation of Wireless Local Area Network<br />
Access Point on BombardierBD-100-<br />
1A10Revision of the <strong>EASA</strong> STC 10030934,<br />
<strong>EASA</strong> Validation of TCAA<br />
approvedSupplemental Type Certificate SA10-<br />
50<br />
10030938 BOMBARDIER AEROSPACE REV. 1 TCCA STC SA10-44 BD100-1A10 CHALLENGER 300 Installation of Mechanical Provisions and LRU<br />
Installation, AircellAir-to-Ground<br />
Communication System and Immarsat Satcom<br />
System.Revision of the <strong>EASA</strong> STC<br />
10030938, validation of TCAA<br />
approvedSupplemental Type Certificate SA10-<br />
44<br />
10033558 BOMBARDIER AEROSPACE REV. 1 TCCA STC SA10-109 CL-600-2B16 Dual Power for Electronic Flight Bag (EFB) -<br />
Challenger 6<strong>04</strong>/605<br />
10033889 BOMBARDIER AEROSPACE TCCA STC NO. SA11-1 ISSUE 1 CL-600-2B16 Activation of Wireless Local Area Network<br />
Acces Point ICG NXT MailServer System<br />
10034212 BOMBARDIER AEROSPACE TCCA STC SA10-93 CL-600-2B16 WLAN Activation & Incorporation of Aircell<br />
Components<br />
10036<strong>04</strong>2 BOMBARDIER AEROSPACE P-<br />
<strong>EASA</strong>.IM.A.S.03247<br />
TCCA STC SA07-110 BOMBARDIER BD-100-1A10<br />
CHALLENGER 300<br />
10037113 BOMBARDIER AEROSPACE REV. 1 TCCA STC SA11-41 BD-100-1A10 (CHALLENGER<br />
300)<br />
Installation of AVS-470 Tail Camera System.<br />
<strong>EASA</strong> Validation of:Transport Canada<br />
Supplemental Type Certificate SA07-110,<br />
Issue 1 dated3rd August 2007 in accordance<br />
with Aero Consulting Services Ltd.Modification<br />
Data Summary F1610<strong>01</strong>.<br />
Activation of Wireless Local Area Network<br />
Access Point, ICG NxtMailServer System<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 />
23.09.2<strong>01</strong>0<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 />
23.09.2<strong>01</strong>0<br />
The complete custom aircraft interior defined Prior to installation of this modification it 11.08.2<strong>01</strong>1<br />
by <strong>EASA</strong> STC No. 10<strong>01</strong>6<strong>01</strong>9must be installed must be determined thatthe<br />
concurrently or as a pre-requisite.<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 />
Structural and electrical provisions must be<br />
installed in accordancewith <strong>EASA</strong> STC No.<br />
10<strong>01</strong>6<strong>01</strong>9 (TCCA STC No. SA06-90)<br />
Structural and electrical provisions must be<br />
installed in accordancewith <strong>EASA</strong> STC No.<br />
10<strong>01</strong>6<strong>01</strong>9 (TCCA STC No. SA06-90)<br />
concurrently or as apre-requisite.<br />
10037705 BOMBARDIER AEROSPACE TCCA STC NO. SA11-89 ISSUE 1 CL-600-2B16 Modification to Potable Water Tank Air Supply Previous installation of a specific potable water<br />
system is required.Drawings listed in<br />
Modification Data Summary H311000 identify<br />
theprerequisite installations.<br />
Prior to installation of this modification it 16.02.2<strong>01</strong>1<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 16.03.2<strong>01</strong>1<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 the 23.07.2009<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 installati<br />
This system is intended to provide cached Structural and electrical provisions must 07.11.2<strong>01</strong>1<br />
internet content and e-mailservices to Portable be installed in accordancewith TCCA<br />
Electronic Devises. Any other use of this STC SA<strong>04</strong>-112 (<strong>EASA</strong> STC 10<strong>01</strong>6423)<br />
equipmentwill require a re-examination of the concurrently or as apre-requisite. Prior to<br />
certificate basis.this STC is a design<br />
installation of this modification it must be<br />
certification approval for the activati<br />
determined thatthe interrelationship<br />
between this modifi<br />
Prior to installation of this modification it 16.12.2<strong>01</strong>1<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> 121/<strong>462</strong>
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