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 />
10027058 BOMBARDIER COMPLETION CENTRE P-<br />
TCCA STC SA<strong>04</strong>-113 BD-700-1A10 Installation, complete Custom Aircraft Interior Restricted to ASN 9306. 1. Refer to the Prior to installation of this modification it 02.09.2009<br />
INC<br />
<strong>EASA</strong>.IM.A.S.03192<br />
Limitations sections of the required AFM must be determined thatthe<br />
Supplement andto the referenced FCOMS. 2. interrelationship between this modification<br />
WLAN system is compatible only to IEEE and any other previouslyinstalled<br />
802.11(b). 3. Prior to installation of this modification and/ or repair will introduce<br />
modification the installer mustdetermine that no adverse effectupon the airworthiness<br />
the<br />
of the product.<br />
10028361 BOMBARDIER COMPLETION CENTRE<br />
INC<br />
10028491 BOMBARDIER COMPLETION CENTRE<br />
INC<br />
10028492 BOMBARDIER COMPLETION CENTRE<br />
INC<br />
TCCA STC SA05-60 BD-700-1A11 Installation, Complete Custom Aircraft Interior -<br />
ASN 9353<br />
Restricted to ASN 9353 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 />
21.12.2009<br />
TCCA STC C-LSA09-091/D BD-700-1A10 Bandit Mask Paint Scheme - ASN 9332. Restricted to ASN 9332. 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 />
15.<strong>01</strong>.2<strong>01</strong>0<br />
TCCA STC SA<strong>04</strong>-113 BD-700-1A10 Installation, Complete Custom Aircraft Interior -<br />
ASN 9332.<br />
10<strong>01</strong>5334 BOMBARDIER INC. <strong>EASA</strong>.IM.A.S.00358 TCCA LTD STC C-LSA<strong>04</strong>-212/D CL-600-2B16 Installation of Securaplane Camera System<br />
Transport Canada Limited STC C-LSA<strong>04</strong>-<br />
212/D in accordance with Aero Consulting<br />
Services Modification Data Summary Notice<br />
E091000 Revision n/c or later Transport<br />
Canada Approved Revision.<br />
10<strong>01</strong>5477 BOMBARDIER INC. <strong>EASA</strong>.IM.A.S.<strong>01</strong>231 C-LSA05-024/D BOMBARDIER BD-700-1A10<br />
BOMBARDIER BD-700-1A11<br />
Installation of Thales Integrated Electronic<br />
Standby Instruments for BD700-1A10 Global<br />
Express and BD700-1A11 Global<br />
5000Validation of imported TCC STC: SA<strong>04</strong>-<br />
118<br />
10<strong>01</strong>5498 BOMBARDIER INC. <strong>EASA</strong>.IM.A.S.<strong>01</strong>261 C-LSA05-298/D BOMBARDIER CL-600-2B16 (CL- Aircraft Completion 11 Passenger Interior<br />
6<strong>04</strong><br />
Configuration<br />
10<strong>01</strong>5499 BOMBARDIER INC. <strong>EASA</strong>.IM.A.S.<strong>01</strong>262 TCCA STC C-LSA05-321/D BOMBARDIER CL-600-2B16 (CL- Aircraft Completion 9 Passenger Interior<br />
6<strong>04</strong><br />
Configuration<br />
10<strong>01</strong>5500 BOMBARDIER INC. <strong>EASA</strong>.IM.A.S.<strong>01</strong>263 C-LSA06-022/D BOMBARDIER CL-600-2B16 (CL- Aircraft Completion, 12 Passenger Interior<br />
6<strong>04</strong><br />
Configuration<br />
10<strong>01</strong>55<strong>01</strong> BOMBARDIER INC. <strong>EASA</strong>.IM.A.S.<strong>01</strong>264 BOMBARDIER BD-100-1A10 Installation of an Executive interior on aircraft<br />
(CHALLE<br />
20<strong>04</strong>7 in accordance with MDL E449000<br />
10<strong>01</strong>5502 BOMBARDIER INC. <strong>EASA</strong>.IM.A.S.<strong>01</strong>265 REV 1 TCCA C-LSA06-051/D BOMBARDIER BD-100-1A10<br />
(CHALLE<br />
Aircraft completion, 9 passengers interior<br />
configuration in accordance with Aero<br />
Consulting Services Ltd. Modification Data<br />
SummaryE840000 Revision N/C<br />
Restricted to ASN 9332.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 />
1. Subject to compliance with the provisions<br />
of Part 21 Subpart E, this STC and associated<br />
data shall remain valid until surrendered,<br />
withdrawn or otherwise terminated.2. If<br />
transfer of this Certificate is requested under<br />
Part 21A.116, the STC will b<br />
1. ref. G-FM340<strong>04</strong>0<strong>01</strong> Rev B2. This STC is<br />
approved only for the product configuration as<br />
defined in the approved design data referred to<br />
in the paragraph "Description". Compatibility<br />
with other aircraft/engine configurations shall<br />
be determined by the<br />
Prior to installation of this modification it 15.<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 />
07.12.20<strong>04</strong><br />
08.08.2005<br />
Valid only for ASN 5596 Registration OY-SGM 07.09.2005<br />
This STC is approved only for the product<br />
15.11.2005<br />
configuration as defined in the approved design<br />
data referred to in the paragraph "Description".<br />
Compatibility with other aircraft/engine<br />
configurations shall be determined by the<br />
installer.<br />
Restricted to ASN 5602 20.<strong>01</strong>.2006<br />
1. This STC is limited to SN 20<strong>04</strong>7.2.<br />
Certification Basis: an equivalent Safety<br />
Finding has been granted in CRI D-8 for<br />
Emergency exit Marker and Locator Signes.A<br />
deviation form paragraph 25.785(B) has been<br />
granted for personal injury criteria of dynamic t<br />
1. This STC is limited to SN 200942. This<br />
STC is approved only for the product<br />
configuration as defined in the approved design<br />
data referred to in the paragraph "Description".<br />
Compatibility with other aircraft/engine<br />
configurations shall be determine<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 126/<strong>462</strong><br />
07.11.2005<br />
02.08.2006
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