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>4764 ACC COLUMBIA JET SERVICE GMBH <strong>EASA</strong>.A.S.02954 LEARJET 35<br />
Installation of Honeywell EGPWS Mk. VIII(in None 02.03.2007<br />
LEARJET 35A<br />
combination with an existing Weather Redar<br />
LEARJET 36<br />
LEARJET 36A<br />
display)<br />
10<strong>01</strong>7178 ACC COLUMBIA JET SERVICE GMBH <strong>EASA</strong>.R.S.<strong>01</strong>296 EUROCOPTER DEUTSCHLAND Installation of a HeliMap.MIDI.P0252 Moving<br />
19.09.2006<br />
EC-135-<br />
Map System<br />
10<strong>01</strong>7179 ACC COLUMBIA JET SERVICE GMBH <strong>EASA</strong>.R.S.<strong>01</strong>297 EUROCOPTER DEUTSCHLAND Installation of a HeliMap MIDI.P0252 Moving<br />
19.09.2006<br />
MBB-BK<br />
Map System<br />
10<strong>01</strong>7213 ACC COLUMBIA JET SERVICE GMBH <strong>EASA</strong>.R.S.<strong>01</strong>369 EUROCOPTER DEUTSCHLAND Installation of an EAE Heli.Map.MDI.P0252<br />
14.06.2007<br />
MBB-BK<br />
system with extension box (for advisory<br />
only).Installation of a moving map system into<br />
BK117B-2 and BK117C-1 models.<br />
10034112 ACC COLUMBIA JET SERVICE GMBH CL-600-2B16, CL-600-2B19 Installation of a combined IRIDIUM-GPS None Prior to installation of this modification it 08.03.2<strong>01</strong>1<br />
Antenna as provision of anoptional Sky<br />
must be determined thatthe<br />
Tracking System.<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>01</strong>4653 ACI SYSTEMES <strong>EASA</strong>.A.S.02810 BEECH 200 ATC replacement and Mode S installation. AFMS must be on board when modified 07.05.2007<br />
10<strong>01</strong>4737 ACI SYSTEMES <strong>EASA</strong>.A.S.02920 CESSNA 550 Single pilot operation and associated<br />
modifications<br />
06.06.2007<br />
10<strong>01</strong>4902 ACI SYSTEMES <strong>EASA</strong>.A.S.03137 REIMS AVIATION CESSNA F 406 ACI-024 - Universal UNS-1L Installation - B- F406 equipped with KCP220 Allied Signal<br />
10.10.2007<br />
RNAV and P-RNAV Capability.<br />
AutoPilot.<br />
10<strong>01</strong>4905 ACI SYSTEMES <strong>EASA</strong>.A.S.03140 REIMS AVIATION CESSNA F 406 ACI-030 - Installation of an NAT NTX138 - FM<br />
Communication device.<br />
08.10.2007<br />
10<strong>01</strong>4996 ACI SYSTEMES <strong>EASA</strong>.A.S.03293 BEECH 90 GNS 430 and B-RNAV capability on Beech 90 N/A 18.02.2008<br />
10<strong>01</strong>5003 ACI SYSTEMES <strong>EASA</strong>.A.S.03303 FALCON 50<br />
FALCON 900<br />
Falcon 50 and F900 EHS Mode S Capability Applicability for Falcon 50 and F900 which are<br />
already Mode A, C and ELS Mode S certified,<br />
ACAS certified and equipped with a dual<br />
transponder system.<br />
10<strong>01</strong>50<strong>04</strong> ACI SYSTEMES <strong>EASA</strong>.A.S.033<strong>04</strong> FALCON 10 Falcon 10 EHS Mode S Capability. Applicabilty for Falcon 10 that are already<br />
Mode A. C and ELS Mode S certified and<br />
equipped with a dual transponder system.<br />
10<strong>01</strong>5<strong>01</strong>6 ACI SYSTEMES <strong>EASA</strong>.A.S.03320 CESSNA 550 ACI-<strong>04</strong>5 - DFDR Upgrade. This STC is only applicable to aircraft equipped<br />
with Fairchild F800 FDR.<br />
10<strong>01</strong>5075 ACI SYSTEMES <strong>EASA</strong>.A.S.03406 BEECH 200<br />
Installation of a Garmin 400 Series with B-<br />
BEECH 300<br />
RNAV capability on Beech 200.<br />
10<strong>01</strong>5099 ACI SYSTEMES <strong>EASA</strong>.A.S.03441 BEECH 90 Installation of Garmin 500 Series GPS with B-<br />
RNAV capability on Beech 90.<br />
10<strong>01</strong>6968 ACROHELIPRO GLOBAL SERVICES,<br />
INC<br />
<strong>EASA</strong>.IM.R.S.<strong>01</strong>369 FAA STC SR02292AK BELL 206<br />
BELL 206A<br />
BELL 206B<br />
BELL 206L<br />
BELL 206L-1<br />
BELL 206L-3<br />
BELL 206L-4<br />
Sagem ICDS and Crossbow AHRS Installation.<br />
Consists of two 8 inch integrated cockpit<br />
display units (one PFD and one MFD) including<br />
engine instruments and an attitude and heading<br />
reference system. This STC is classified as<br />
"BASIC" by the FAA and is approved<br />
10031149 ACS-NAI Ltd. TCCA STC SA10-26 CL-600-2B19 Installation, CMC Electronics Pilot view Class II<br />
Electronics Flight Bag<br />
The supplemental Airplane Flight Manual ACI-<br />
09-AFM-M-070, revision 0, dated 15 January<br />
2008 must be on board when the modification<br />
is installed.<br />
Maximum ambient operating temperature of 40<br />
degrees Celsius (103 degrees Fahrenheit)<br />
29.10.2007<br />
29.10.2007<br />
16.05.2008<br />
05.02.2008<br />
<strong>04</strong>.<strong>04</strong>.2008<br />
31.10.2007<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 />
29.07.2<strong>01</strong>0<br />
10031944 ACS-NAI Ltd. TCCA STC #C-LSA10-034/D ISS 1 BD-700-1A10 Installation of Two 16G Side Facing Divans Restricted to ASN 9347 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 />
23.09.2<strong>01</strong>0<br />
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