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>6657 BOMBARDIER AEROSPACE <strong>EASA</strong>.IM.A.S.03117 TCCA C-LSA09-0002/D ISSUE 1 BOMBARDIER CL-600-2B16 Main & Nose Wheel Storage Modifications. 1. Restricted to ASN 5426.2. Prior to<br />
installation of this modification the installer must<br />
determine that the interrelationship between<br />
this modification and any other previously<br />
installed modification will introduce no adverse<br />
effect upon the airwor<br />
20.<strong>01</strong>.2009<br />
10<strong>01</strong>6671 BOMBARDIER AEROSPACE <strong>EASA</strong>.IM.A.S.03161 TCCA STC SA09-16 BD-100-1A10 (CHALLENGER Installation of KGS Electronic SS200 Static Prior to installation of this modification the<br />
06.<strong>04</strong>.2009<br />
300)<br />
Inverter<strong>EASA</strong> Validation of:Transport Canada installer must determine that the<br />
Supplemental Type Certificate SA09-16, Issue interrelationship between this modification and<br />
2 dated19th March 2009 in accordance with any other previously installed modification<br />
Aero Consulting Services Ltd. Modification will introduce no adverse effect upon the<br />
Data Summary G072000 Revision B. airworthiness of the product.<br />
10<strong>01</strong>6673 BOMBARDIER AEROSPACE <strong>EASA</strong>.IM.A.S.03176 TCCA STC SA<strong>04</strong>-69 ISSUE 1 BOMBARDIER BD-100-1A10<br />
(CHALLE<br />
10<strong>01</strong>6676 BOMBARDIER AEROSPACE <strong>EASA</strong>.IM.A.S.03189 FAA STC ST02683CH BOEING 747-400 SERIES Installation of EZMount (TM) mechanical<br />
mounting assembly on lower frame of cockpit<br />
sliding windows in accordance with Electronic<br />
Cable Specialists Master Data List ECS-<br />
206728 Rev. E, dated April 8, 2009, or later<br />
FAA approved revisions.Validation of FAA S<br />
10027267 BOMBARDIER AEROSPACE P-<br />
<strong>EASA</strong>.IM.A.S.03252<br />
TCCA STC SA09-43 BD-100-1A10 (CHALLENGER<br />
300)<br />
Installation of 115 VAC TIA Wavejet<br />
1. Prior to installation of this modification the<br />
Microwave Oven in Forward RH Galley.<strong>EASA</strong> installer must determine that the<br />
Validation of:Transport Canada Supplemental interrelationship between this modification and<br />
Type Certificate SA<strong>04</strong>-69, Issue 1 dated 4th any other previously installed modification will<br />
June 20<strong>04</strong> in accordance with Aero Consulting introduce no adverse effect upon the<br />
Services Ltd. Modification Data Summary airworthiness of the product.2.<br />
E02700<br />
VHF COMM 3 Power Source Relocation<strong>EASA</strong><br />
Validation of:Transport Canada Supplemental<br />
Type Certificate SA09-43, Issue 1 dated20th<br />
May 2009 in accordance with Aero Consulting<br />
Services Ltd.Modification Data Summary<br />
F912000 Revision N/C.<br />
1. AFM Supplement as listed in Appendix A of<br />
Electronic Cable Specialists Master Data List<br />
ECS-206728, Rev. E, dated April 8, 2009 or<br />
later FAA approved revision, is required on<br />
board the modified aircraft.2. The equipment<br />
for which these provisions are in<br />
<strong>04</strong>.05.2009<br />
18.06.2009<br />
None 1) Prior to installation of this modification 17.09.2009<br />
the installer mustdetermine that the<br />
interrelationship between this modification<br />
and anyother previously installed<br />
modification will introduce no adverse<br />
effectupon the airworthiness of the<br />
product. 2) The inst<br />
10027876 BOMBARDIER AEROSPACE TCCA STC SA09-53 ISSUE 1 CL-600-2B16 Optional Fuel Quantity Display in Kilograms Not Applicable. 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 />
11.11.2009<br />
10028730 BOMBARDIER AEROSPACE TCCA LSTC C-LSA08-338/D CL-600-2B16 Installation, Complete Custom Aircraft Interior -<br />
ASN 5506<br />
10029282 BOMBARDIER AEROSPACE TCCA STC SA10-21 CL-600-2B16 Installation, Un-Upholstered Headliner,<br />
Rockwell Collins HUD.<br />
Restricted to ASN 5506.Aircraft must be fitted<br />
with an approved means to disconnect the<br />
cabinAC and DC utility buses as a prerequisite<br />
to this modification.<br />
Prior to installation of this modification it 05.02.2<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 />
17.03.2<strong>01</strong>0<br />
10029957 BOMBARDIER AEROSPACE TCCA STC SA10-36 CL-600-2B16 Installation, Quick Access Recorder (QAR) 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 />
06.05.2<strong>01</strong>0<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 120/<strong>462</strong>
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