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>04</strong>1500 BOMBARDIER INC. REV. 1 TCCA STC SA-12-16 ISSUE 2 BD-700-1A10 Installation, Aircraft Completion Modifications - Restricted to ASN 9464 Prior to installation of this modification it 24.09.2<strong>01</strong>2<br />
ASN 9464<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>04</strong>1512 BOMBARDIER INC. TCCA STC SA-12-16 ISSUE 2 BD-700-1A11 Installation, Aircraft Completion Modifications -<br />
ASN 9<strong>462</strong><br />
10<strong>04</strong>1975 BOMBARDIER INC. TCCA STC NO. SA12-16 BD-700-1A11 Installation, Aircraft Completion Modifications -<br />
ASN 9458.<br />
10<strong>04</strong>2314 BOMBARDIER INC. TCCA STC NO. SA12-16 BD-700-1A10<br />
BD-700-1A11<br />
10<strong>04</strong>2835 BOMBARDIER INC. STC NO C-LSA03-348/D BD-700-1A10 Aircraft Completion, 13 Passenger Interior<br />
Configuration<br />
10<strong>01</strong>6316 BOMBARDIER INC. - COMPLETION<br />
CENTRE<br />
10029547 BOMBARDIER SHORTS BROTHERS,<br />
PLC<br />
<strong>EASA</strong>.IM.A.S.02622 REV. 7 TCCA STC SA07-119 BD100 CHALLENGER 300 Installation, In-Service Improvement<br />
Restricted to ASN 9<strong>462</strong>. 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 />
24.09.2<strong>01</strong>2<br />
Restricted to ASN 9458. The Wireless Local<br />
Area Network (WLAN) is intended to provide<br />
internetconnectivity and email services to the<br />
airplane's cabin using portableelectronic<br />
devices (PEDs).Any other intended function of<br />
this equipment will require are-exa<br />
Installation, Aircraft Completion Modifications. <strong>EASA</strong> approved configurations are identified in<br />
Configuration DefinitionRecord RAZ-BM700-<br />
0<strong>01</strong>. The Wireless Local Area Network<br />
(WLAN) is intended to provide<br />
internetconnectivity and email services to the<br />
airplane’s cabin using portableelectronic<br />
devices (PED<br />
ModificationsIn-service design improvements to<br />
cabin interior featuresRevision of the <strong>EASA</strong><br />
STC 10<strong>01</strong>6316, Rev. 6 due to revised<br />
technicaldata (Modification Data Summary<br />
F344000 Rev. H )<br />
P-<strong>EASA</strong>.A.S.03579 A319, A320, A321SERIES V2500 NACELLE - RTI MONOLITHIC FAN<br />
COWL DOOR<br />
1003<strong>04</strong>74 BOND HELICOPTERS EUROPE Ltd. EC135 T2(CPDS), EC135 T2+ Engine Usage Monitoring SystemInstallation of<br />
an Engine Usage Monitoring System in<br />
accordance withchange number<br />
BOND/MOD/<strong>01</strong>0 as defined in DL/<strong>01</strong>0-099 to<br />
monitor certainengine parameters, further<br />
described in Design Report DR/<strong>01</strong>0-0<strong>01</strong>.<br />
10031949 BOND HELICOPTERS EUROPE Ltd. REV. 1 AS 332 L2 Installation of TCAS II system in accordance<br />
with BOND/MOD/<strong>01</strong>8.<br />
Restricted to ASN 9093.Bombardier Service<br />
Bulletin 700-31-<strong>01</strong>8 Modification -<br />
IntegratedAvionics Computers - Avionics 20<strong>01</strong><br />
Batch 1 IAC Upgrade must be embodied.<br />
Prior to installation of this modification it 29.10.2<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 />
Prior to installation of this modification it 23.11.2<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 />
Prior to installation of this modification it 20.12.2<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 />
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 />
28.10.2<strong>01</strong>0<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 />
31.03.2<strong>01</strong>0<br />
None It is the operator's responsibility to obtain 17.06.2<strong>01</strong>0<br />
operational approval forthe use of the<br />
system in accordance with the operating<br />
rules of theapplicable civil aviation<br />
authority.Prior to installation of this<br />
modification it must be determined<br />
thatthe interrelat<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 />
06.07.2<strong>01</strong>1<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 139/<strong>462</strong>
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