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>6237 BOMBARDIER AEROSPACE <strong>EASA</strong>.IM.A.S.025<strong>01</strong> TCCA STC C-LSA07-366/D BD-100-1A10 (CHALLENGER AIRCRAFT COMPLETION, 10<br />
This STC is limited to aircraft Bombardier<br />
10.<strong>01</strong>.2008<br />
300)<br />
PASSENGERS INTERIOR CONFIGURATION BD100-1A10 Serial Number 2<strong>01</strong>69.<br />
/<strong>EASA</strong> Validation of:Transport Canada Limited<br />
Supplemental Type Certificate C-LSA07-<br />
366/DIssue 1 dated 20th December 2007, in<br />
accordance with Aero ConsultingServices Ltd.<br />
Modification Data Summary F<br />
10<strong>01</strong>6238 BOMBARDIER AEROSPACE <strong>EASA</strong>.IM.A.S.02502 TCCA STC C-LSA07-320/D BD-100-1A10 (CHALLENGER<br />
300)<br />
10<strong>01</strong>6362 BOMBARDIER AEROSPACE <strong>EASA</strong>.IM.A.S.02684 TCCA STC C-LSA08-<strong>01</strong>4/D BD-100-1A10 (CHALLENGER<br />
300)<br />
AIRCRAFT COMPLETION, 10<br />
This STC is limited to aircraft Bombardier<br />
PASSENGERS INTERIOR CONFIGURATION BD100-1A10 Serial Number 2<strong>01</strong>59.<br />
/<strong>EASA</strong> Validation of:Transport Canada Limited<br />
Supplemental Type Certificate C-LSA07-<br />
320/DIssue 1 dated 20th November 2007, in<br />
accordance with Aero ConsultingServices Ltd.<br />
Modification Data Summary F5<br />
AIRCRAFT COMPLETION, 10<br />
This STC is limited to aircraft Bombardier<br />
PASSENGERS INTERIOR CONFIGURATION BD100-1A10 Serial Number 2<strong>01</strong>79.<br />
/<strong>EASA</strong> Validation of:Transport Canada Limited<br />
Supplemental Type Certificate C-LSA08-<br />
<strong>01</strong>4/DIssue 1 dated 20th February 2008, in<br />
accordance with Aero ConsultingServices Ltd.<br />
Modification Data Summary F<br />
10<strong>01</strong>6423 BOMBARDIER AEROSPACE <strong>EASA</strong>.IM.A.S.02761 REV. 35 TCCA STC SA<strong>04</strong>-112 BD100-1A10 (CHALLENGER 300) Customized Interior CompletionNote: Major The revised STC is limited to aircraft<br />
Change to <strong>EASA</strong> STC 10<strong>01</strong>6423 rev 34 which Bombardier BD100-1A10 SerialNumber<br />
has been updated toinclude S/N 20357 20096, 20200, 20206, 20214, 20218, 20221,<br />
20222, 20226, 20227,<br />
20232,20236,20237, 20241, 20243,<br />
20251, 20252, 20256, 20261, 20271, 20272,<br />
20274,20275,20276, 20277, 20284,<br />
10<strong>01</strong>6476 BOMBARDIER AEROSPACE <strong>EASA</strong>.IM.A.S.02826 REV. 2 TCCA STC SA08-35 ISSUE 3 BD100-1A10 (CHALLENGER 300) Observer Seat Installation, Model 409-00<strong>01</strong><br />
/Installation of an observer seat between the<br />
avionics racks, forward ofthe main passenger<br />
cabin.Revision of <strong>EASA</strong> STC 10<strong>01</strong>6476, Rev.<br />
1 due to revised technical data(Modification<br />
Data Summary F797000 Rev. D).<br />
26.11.2007<br />
25.02.2008<br />
Prior to installation of this modification it 16.07.2<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 />
Observer Seat for crew use only 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.<strong>01</strong>.2<strong>01</strong>1<br />
10<strong>01</strong>6477 BOMBARDIER AEROSPACE <strong>EASA</strong>.IM.A.S.02828 TCCA STC SA08-58 ISSUE 1 CL-600-2B16 (6<strong>04</strong>) Installation, AVS-470 Tail Camera System 1. For Configuration -2, the modification<br />
defined by <strong>EASA</strong> STC No.<br />
<strong>EASA</strong>.IM.A.S.<strong>01</strong>946 (TCCA STC No. SA97-<br />
71) must be embodied as aprerequisite.2.<br />
Prior to installation of this modification the<br />
installer must determine that the<br />
interrelationship between<br />
<strong>01</strong>.10.2008<br />
10<strong>01</strong>6493 BOMBARDIER AEROSPACE <strong>EASA</strong>.IM.A.S.02855 TCCA C-LSA08-097/D ISSUE 1 CL-600-2B16 Installation of Club Seating 05.05.2008<br />
10<strong>01</strong>6494 BOMBARDIER AEROSPACE <strong>EASA</strong>.IM.A.S.02856 TCCA C-LSA07-418/D ISSUE 1 BOMBARDIER CL-600-2B16 (6<strong>04</strong>) Installation of EMS High Speed Data System 1. Restricted to ASN 54642. Limitation: This<br />
approval is limited to 1,500 flight cycles or 12<br />
months from the approval date, whichever<br />
comes first until theAirworthiness Limitations<br />
subdocument BAS63<strong>01</strong><strong>01</strong>16-AWL-1 of<br />
Bombardier IFCA BAS63<strong>01</strong><strong>01</strong>16-IFCA-1 is<br />
app<br />
28.07.2008<br />
10<strong>01</strong>6502 BOMBARDIER AEROSPACE <strong>EASA</strong>.IM.A.S.02865 TCCA STC C-LSA08-237/D BD-100-1A10 (CHALLENGER<br />
300)<br />
10<strong>01</strong>6631 BOMBARDIER AEROSPACE <strong>EASA</strong>.IM.A.S.03068 TCCA STC C-LSA08-275/D ISS1 BD-100-1A10 (CHALLENGER<br />
300)<br />
CUSTOMIZED INTERIOR COMPLETION – 1 Prior to installation of this modification the<br />
AIRCRAFT 2021210 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-LSA08-237/DIssue 1 dated 24th September introduce no adverse effect upon the<br />
2008, in accordance with Aero<br />
ConsultingServices Ltd<br />
airworthiness of the product.1 Th<br />
Customized Interior Completion - Aircraft Prior to installation of this modification the<br />
200659 passenger seats interior<br />
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<br />
C-LSA08-275/DIssue 1 dated 21st October will introduce no adverse effect upon the<br />
2008, in accordance with Aero<br />
ConsultingServices Ltd.<br />
airworthiness of the product.<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 119/<strong>462</strong><br />
09.10.2008<br />
06.11.2008