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>6332 BOMBARDIER INC. <strong>EASA</strong>.IM.A.S.02641 REV. 1 TCCA STC C-LSA07-229/D BD-700-1A11 Installation, Interior Completions In-Service Restricted to ASN 9249 Prior to installation of this modification it 20.<strong>04</strong>.2<strong>01</strong>1<br />
Improvement Modificationsfor ASN 9249.<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<strong>01</strong>6333 BOMBARDIER INC. <strong>EASA</strong>.IM.A.S.02642 TCCA STC NO. SA<strong>04</strong>-112 ISSUE 3. BOMBARDIER BD-100-1A10<br />
(CHALLE<br />
10<strong>01</strong>6427 BOMBARDIER INC. <strong>EASA</strong>.IM.A.S.02766 TCCA STC C-LSA08-145/D ISSUE 1 BOMBARDIER BD-100-1A10<br />
(CHALLE<br />
10<strong>01</strong>6446 BOMBARDIER INC. <strong>EASA</strong>.IM.A.S.02792 STC C-LSA08-107/D BOMBARDIER BD-100-1A10<br />
(CHALLE<br />
10<strong>01</strong>6478 BOMBARDIER INC. P-<br />
<strong>EASA</strong>.IM.A.S.02830<br />
REV. 4 TCCA STC SA<strong>04</strong>-113 BD-700-1A10 Aircraft Completion, 13 Passenger Interior<br />
Configuration<br />
10<strong>01</strong>6544 BOMBARDIER INC. <strong>EASA</strong>.IM.A.S.02923 REV. 5 TCCA STC SA08-48 BD-700-1A10, BD-700-1A11 Installation, Interior Completions In-Service<br />
Improvement Modifications<br />
AIRCRAFT COMPLETION, 10<br />
This STC is limited to aircraft Bombardier<br />
PASSENGERS INTERIOR CONFIGURATION BD100-1A10 Serial Number 2<strong>01</strong>41.<br />
/<strong>EASA</strong> Validation of:Transport Canada Limited<br />
Supplemental Type Certificate C-LSA07-<br />
411/DIssue 1 dated 5th December 2007, in<br />
accordance with Aero ConsultingServices Ltd.<br />
Modification Data Summary F63<br />
10<strong>01</strong>6660 BOMBARDIER INC. <strong>EASA</strong>.IM.A.S.03121 REV. 1 TCCA STC SA05-60 BD-700-1A11 Installation, Complete Custom Aircraft Interior<br />
(S/N 9311).<br />
CUSTOMIZED INTERIOR COMPLETION – Prior to installation of this modification the<br />
AIRCRAFT 2020310 passenger seats interior installer must determine that the<br />
configuration<strong>EASA</strong> Validation of:Transport interrelationship between this modification and<br />
Canada Limited Supplemental Type Certificate any other previously installed modification will<br />
C-LSA08-145/DIssue 1 dated 18th August introduce no adverse effect upon the<br />
2008, in accordance with Aero<br />
airworthiness of the product.1 The ins<br />
ConsultingServices Ltd. M<br />
AIRCRAFT COMPLETION, 10<br />
This STC is limited to aircraft Bombardier<br />
PASSENGERS INTERIOR CONFIGURATION BD100-1A10 Serial Number 2<strong>01</strong>23.<br />
/<strong>EASA</strong> Validation of:Transport Canada Limited<br />
Supplemental Type Certificate C-LSA08-<br />
107/DIssue 1 dated 19th March 2008, in<br />
accordance with Aero ConsultingServices Ltd.<br />
Modification Data Summary F786<br />
Restricted to ASN 9274 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 />
10027337 BOMBARDIER INC. TCCA STC SA<strong>04</strong>-113 BOMBARDIER BD-700-1A10 Installation, Complete Custom Aircraft Interior Restricted to ASN 9309.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 />
10027762 BOMBARDIER INC. REV. 1 TCCA STC SA05-60 BD-700-1A11 Installation, Complete Custom Aircraft Interior -<br />
ASN 9343<br />
Prior to installation of this modification the<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 />
18.12.2007<br />
20.08.2008<br />
28.03.2008<br />
12.<strong>04</strong>.2<strong>01</strong>1<br />
None<br />
product.<br />
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 />
11.05.2<strong>01</strong>1<br />
Restricted to ASN 9311. 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 />
<strong>04</strong>.06.2<strong>01</strong>0<br />
Prior to installation of this modification it 22.09.2009<br />
must be determined thatthe<br />
interrelationship between this modification<br />
and any other previouslyinstalled<br />
modification will introduce no adverse<br />
effect upon theairworthiness of the<br />
product.<br />
Restricted to ASN 9343. 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 />
<strong>04</strong>.06.2<strong>01</strong>0<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 129/<strong>462</strong>
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