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>5563 BOMBARDIER INC. <strong>EASA</strong>.IM.A.S.<strong>01</strong>461 TCCA STC Q-LSA05-030/D BD-700-1A10 Installation of Replacement Cockpit Printer 1. Installation is limited to S/N 9086Note: All<br />
Portable Electronic Equipment/Devices PED,<br />
must be unplugge, turned-off and stowed prior<br />
taxi, take-off and landing2. This STC is<br />
approved only for the product configuration as<br />
defined in the approved design<br />
12.12.2005<br />
10<strong>01</strong>5591 BOMBARDIER INC. <strong>EASA</strong>.IM.A.S.<strong>01</strong>502 TCCA LIMITED STC C-LSA05-347/D BOMBARDIER BD-700-1A10 Installation, Aircraft Interior Completion for<br />
BD700-1A10 Global Expressacc.: MDS<br />
E583000 Rev. N/CValidation of imported<br />
TCCA Limited STC: C-LSA05-347/D<br />
ref. G-FM2500<strong>01</strong>33 Rev. N/C; Limited to S/N<br />
9163Note: 1. The airplane is limited to privat<br />
use only unless the mid cabin door is rendered<br />
inoperable.2. Approval of EFB installation does<br />
not constituete operational approval to use<br />
EFB function.3. This STC<br />
10<strong>01</strong>5594 BOMBARDIER INC. <strong>EASA</strong>.IM.A.S.<strong>01</strong>507 FAA STC SA556NE CL-600-2B16 Installation of a Forward Overboard Servicing Limited to Airplane Serial Number 5055 25.10.2005<br />
10<strong>01</strong>5630 BOMBARDIER INC. <strong>EASA</strong>.IM.A.S.<strong>01</strong>582 REV. 1 TCCA STC SA<strong>04</strong>-113 BD-700-1A10 Installation, Completion of custom Aircraft<br />
Interior for BD700-1A10 Global Expressacc.:<br />
CDL D954000 Rev. KValidation of imported<br />
TCC STC: SA<strong>04</strong>-113<br />
1. Ref. G-FM250<strong>04</strong>0<strong>01</strong> Rev. N/C: Limited to<br />
S/N 91452. This STC is approved only for<br />
the product configuration as defined in the<br />
approved design data referred to in the<br />
paragraph "Description". Compatibility with<br />
other aircraft/engine configurations sh<br />
10<strong>01</strong>5641 BOMBARDIER INC. <strong>EASA</strong>.IM.A.S.<strong>01</strong>605 TCCA STC C-LSA06-<strong>01</strong>4/D BOMBARDIER BD-700-1A11 Installation 13 Passenger interior completion for 1. Installation of limited to S/N 91682. This<br />
BD700-1A11<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 determined<br />
10<strong>01</strong>5642 BOMBARDIER INC. <strong>EASA</strong>.IM.A.S.<strong>01</strong>606 REV. 1 TCCA STC C-LSA05-391/D BD-700-1A10 Aircraft Completion, 13 Passenger Interior<br />
Configuration<br />
17.11.2005<br />
12.09.2005<br />
30.<strong>01</strong>.2006<br />
1. This STC is approved only for the product Prior to installation of this modification it 07.07.2<strong>01</strong>0<br />
configuration as defined inthe approved design must be determined thatthe<br />
data referred to in the paragraph<br />
interrelationship between this modification<br />
"Description".Compatibility with other and any other previouslyinstalled<br />
aircraft/engine configurations shall<br />
modification and/ or repair will introduce<br />
bedetermined by the installer.2. The installation no adverse effectupon the airworthiness<br />
is l<br />
of the product.<br />
10<strong>01</strong>5643 BOMBARDIER INC. <strong>EASA</strong>.IM.A.S.<strong>01</strong>607 TCCA STC NO C-LSA05-382/D BOMBARDIER BD-700-1A11 Aircraft Completion 13 Passenger Interior<br />
Configurationalidation of TCCA Limited STC C-<br />
LSA05-382/D to S/N 9170MDL: E810000 Rev<br />
A or later approved revisions<br />
07.<strong>04</strong>.2006<br />
10<strong>01</strong>5675 BOMBARDIER INC. <strong>EASA</strong>.IM.A.S.<strong>01</strong>656 FAA STC ST03065AT LEARJET 31A Installation of a Single Universal UNS-1C+ or<br />
UNS-1E Flight Management System<br />
<strong>04</strong>.<strong>01</strong>.2006<br />
10<strong>01</strong>5737 BOMBARDIER INC. <strong>EASA</strong>.IM.A.S.<strong>01</strong>761 BOMBARDIER BD-700-1A10 Customised Interior Completion Aircraft 20071, 1. S/N 20071<br />
in accordance with Aero Consulting Services<br />
Ltd. Modification Data Summary E725000 rev<br />
N/C or later approved revision<br />
30.<strong>01</strong>.2006<br />
10<strong>01</strong>5743 BOMBARDIER INC. <strong>EASA</strong>.IM.A.S.<strong>01</strong>767 FAA STC ST00393DE-D LEARJET 31A Installation of a Honeywell 440, 660 or 880<br />
Radar System<br />
None 20.<strong>01</strong>.2006<br />
10<strong>01</strong>5781 BOMBARDIER INC. <strong>EASA</strong>.IM.A.S.<strong>01</strong>827 TCCA LTD STC C-LSA06-132/D BOMBARDIER BD-700-1A10 Customized Interior Completion ACSN Aerworthiness Limitations - Camera Sysem<br />
17.07.2006<br />
9173Validation of TCCA Limited STC C- Electrical Receptacle Installation - FS806: G-<br />
LSA06-132/D to S/N 9173MDL: E776000 Rev. TM05100073 Rev. NC or later TCCA<br />
NC or later TCCA approved revisionsTCCA<br />
SoC: C-06-316 dated June 30, 2006<br />
approved revisions<br />
10<strong>01</strong>5841 BOMBARDIER INC. <strong>EASA</strong>.IM.A.S.<strong>01</strong>936 - BOMBARDIER BD-100-1A10 Aircraft completion, interior configuration in Limited to S/N 20097 17.08.2006<br />
(CHALLE<br />
accordance with Aero Consultung Services Ltd.<br />
Modification Data Summary E843000 revision<br />
N/C<br />
10<strong>01</strong>5858 BOMBARDIER INC. <strong>EASA</strong>.IM.A.S.<strong>01</strong>962 TCCA STC C-LSA06-020/D BOMBARDIER BD-100-1A10 Aircraft completion, 10 Passenger interior<br />
configuration, in accordance with MDS<br />
E790000<br />
S/N 20079 24.<strong>04</strong>.2006<br />
10<strong>01</strong>5903 BOMBARDIER INC. <strong>EASA</strong>.IM.A.S.02029 TCCA STC Q-LSA06-25/D BOMBARDIER BD-700-1A10 Installation Acoustic Insulation ACSN<br />
This STC is approved only for the product<br />
25.07.2006<br />
9163Validation of TCCA Limited STC Q- configuration as defined in the approved design<br />
LSA06-25/D to S/N 9163MDL: 26118002 Rev data referred to in the paragraph "Description".<br />
NC or later TCCA approved revisionsTCCA Compatibility with other aircraft/engine<br />
SoC: NAI5<strong>01</strong>2-06-00062 dated June 20, 2006 configurations shall be determined by the<br />
installer.<br />
10<strong>01</strong>5912 BOMBARDIER INC. <strong>EASA</strong>.IM.A.S.02<strong>04</strong>1 C-LSA06-270/D BOMBARDIER BD-100-1A10 Aircraft completion, 10 passenger interior Limited to S/N 2<strong>01</strong>06 18.10.2006<br />
(CHALLE<br />
configuration, in accordance with MDS<br />
F029000 (Original STC numer: Transport<br />
Canada STC C-LSA06-270/D)<br />
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