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 />
10032060 RUAG AEROSPACE SERVICES GmbH CL-600-1A11<br />
Installation of Satcom Iridium System none Prior to installation of this modification it 06.10.2<strong>01</strong>0<br />
CL600-2B16, CL-600-2A12 Simphone DUO<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 />
10032061 RUAG AEROSPACE SERVICES GmbH CL-600-1A11<br />
CL600-2B16, CL-600-2A12<br />
Electronic Flight Bag NavAero tBagC2 (EFB) -<br />
Class II<br />
10033641 RUAG AEROSPACE SERVICES GmbH P-<strong>EASA</strong>.A.S.03896 EMB-135BJ Modification 289A: Thrane & Thrane Aero SB<br />
Lite Satcom Installation<br />
10034074 RUAG AEROSPACE SERVICES GmbH 525<br />
525A<br />
10036250 RUAG AEROSPACE SERVICES GmbH BD 100-1A10 (CHALLENGER<br />
300)<br />
10036633 RUAG AEROSPACE SERVICES GmbH REV. 1 BD-700-1A10<br />
BD-700-1A11<br />
Installation of High Speed SATCOM system<br />
with on-board WLAN Interface.<br />
Installation of EGPWS MK-V with Runway<br />
Awareness and Advisory System(RAAS).<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 />
06.10.2<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 />
<strong>01</strong>.02.2<strong>01</strong>1<br />
STC limited to S/N 525-0516The WLAN clients Prior to installation of this modification it <strong>04</strong>.03.2<strong>01</strong>1<br />
(Handsets, Laptops, etc) are not covered by must be determined thatthe<br />
this STC.The usage of these components is interrelationship between this modification<br />
requiring operational approval.<br />
and any other<br />
previouslyinstalledmodification and/ or<br />
repair will introduce no adverse effect<br />
upon theairworthiness 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 />
25.08.2<strong>01</strong>1<br />
Dual Electronic Flight Bag (EFB) Installation 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 />
27.09.2<strong>01</strong>1<br />
10039078 RUAG AEROSPACE SERVICES GmbH BELL 205A-1 Title: Load Attachment Device BRD<strong>01</strong> on Bell None<br />
205A-1Description: The BRD<strong>01</strong> is a cabin<br />
mounted device for attaching loads onBell<br />
helicopters. It is used with opened sliding doors<br />
and can bemounted left- and righthand<br />
simultaneously.<br />
None <strong>04</strong>.<strong>04</strong>.2<strong>01</strong>2<br />
10<strong>04</strong>2290 RUAG AEROSPACE SERVICES GmbH REV. 1 CL-600-1A11, CL-600-2A12<br />
CL-600-2B16<br />
10<strong>04</strong>2291 RUAG AEROSPACE SERVICES GmbH CL-600-1A11, CL-600-2A12<br />
CL-600-2B16<br />
Flight Management System NZ-2000 -<br />
Upgrade to SW 6.1<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 />
21.11.2<strong>01</strong>2<br />
ACSS TCAS II / 2000 Change 7.1 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 />
21.11.2<strong>01</strong>2<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 382/<strong>462</strong>
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