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>09<strong>01</strong> ELECTRONIC CABLE SPECIALISTS, Inc. FAA STC ST02907CH B747-400<br />
Installation of ECS EZMount mechanical The equipment for which these provisions are AFM Supplement ECS 208936 for 02.08.2<strong>01</strong>2<br />
B747-400F<br />
mounting assemblies in accordancewith installed has not beencertified. Additional Boeing 747-400 series Aircraft<br />
Electronic Cable Specialists, Inc. Master Data approval is required for the installation of equippedwith ECS EZMount tilt is<br />
List ECS 209135,Revision H, dated November thisequipment and must be evaluated to assure required on board of the modified<br />
29, 2<strong>01</strong>1 or later approved revisionValidation of satisfactory compliance withapplicable aircraft.Prior to installation of this<br />
FAA STC ST02907CH<br />
airworthiness standards.<br />
modification it must be determined<br />
thatthe interrelationship between this<br />
modification an<br />
10<strong>04</strong>1328 ELECTRONIC CABLE SPECIALISTS, Inc. FAA STC ST02961CH B737-600/-700/-800/-900/-900ER Validation of FAA STC ST02961CH - None 1) Prior to installation of this STC it must 07.09.2<strong>01</strong>2<br />
Approved configurations are thefollowing:-<br />
be determined that theinterrelationship<br />
Configuration 1: Replacement of Honeywell<br />
between this STC and any other<br />
Weather Radar System RDR-4Bwith<br />
previously installedmodification and / or<br />
Honeywell Honeywell Weather Radar RDR-<br />
repair will introduce no adverse effect<br />
4000,-Configuration 2: Software<br />
upon theairworthiness of the product. 2)<br />
upgrade to Honeywell WRS RDR-4<br />
This STC is <strong>EASA</strong><br />
10<strong>04</strong>2532 ELECTRONIC CABLE SPECIALISTS, Inc. FAA STC ST02992CH B737-600/-700/-800/-900/-900ER Validation of FAA STC ST02992CH -<br />
Installation of dual Electronic FlightBag (EFB)<br />
System Provisions.<br />
10<strong>01</strong>3942 ELECTRONIQUE MAINTENANCE<br />
AVIATION<br />
10<strong>01</strong>3968 ELECTRONIQUE MAINTENANCE<br />
AVIATION<br />
10<strong>01</strong>4112 ELECTRONIQUE MAINTENANCE<br />
AVIATION<br />
10<strong>01</strong>4251 ELECTRONIQUE MAINTENANCE<br />
AVIATION<br />
10<strong>01</strong>4341 ELECTRONIQUE MAINTENANCE<br />
AVIATION<br />
10<strong>01</strong>4747 ELECTRONIQUE MAINTENANCE<br />
AVIATION<br />
10<strong>01</strong>4812 ELECTRONIQUE MAINTENANCE<br />
AVIATION<br />
<strong>EASA</strong>.A.S.00378 REV. 1 FAIRCHILD SWEARINGEN SA<br />
226-T(<br />
- Installation of VHF 8.33<br />
KHz/VOR/ILS/GPS/STORMSCOPE/VHF 150<br />
MHz/UHF/ICS Passengers according to<br />
E.M.A. Modification Approval Sheet (FAM) No<br />
EMA/03/002/SA226Serie/VHF.GPSBRNAV.S<br />
TORM.UHF dated 22 December 2003.-<br />
Installation of GARMIN GNS 530A, STORM<br />
1) The aircraft operator must perform the<br />
instructions for continuedairworthiness and<br />
comply with the Airworthiness Limitation Items<br />
as perthe Instructions for Continued<br />
Airworthiness (ICA), ReferenceECS-209337,<br />
Revision G, dated 22 August 2<strong>01</strong>2. 2) Additio<br />
1. This modification is applicable only to SA<br />
226 T(B) s/n T298 F-GLPT.2. <strong>EASA</strong><br />
Approved Airplane Flight Manual Supplements<br />
"Supplément au manuel de vol GPS BRNAV"<br />
are required.3. This STC is approved only for<br />
the product configuration as defined i<br />
1) Prior to installation of this STC it must<br />
be determined that theinterrelationship<br />
between this STC and any other<br />
previously installedmodification and / or<br />
repair will introduce no adverse effect<br />
upon theairworthiness of the product. 2)<br />
This STC is <strong>EASA</strong><br />
<strong>EASA</strong>.A.S.00738 REV. 1 FAIRCHILD SWEARINGEN SA Installation of GPS BRNAV, EGPWS, TAS, 1. This STC is limited to MSN T312 F-GRNT2.<br />
20.02.2006<br />
226-T(<br />
Stormscope, Radar, MFD- Garmin GNS 530 This STC is approved only for the product<br />
VHF.NAV.GPS, Honeywell RDR 2000 Radar, configuration as defined in the approved design<br />
BF Goodrich WX 500 Stormscope and Avidyne data referred to in the paragraph "Description".<br />
EX 500 MDF installation- BF Goodrich Sky 899 Compatibility with other aircraft/engine<br />
TAS and Honeywell KGP 560 EGPWS<br />
provision<br />
configurations shall be determin<br />
<strong>EASA</strong>.A.S.<strong>01</strong>217 BEECH C90<br />
Allied Signal KT73 ATC Mode S, Kannad This STC is limited to Beech C90 MSN LJ667<br />
13.06.2005<br />
BEECH E90<br />
406AF ELT 406 and 2 IDC 570 altimeters<br />
installation.<br />
& Beech E90 MSN LW 278.<br />
<strong>EASA</strong>.A.S.<strong>01</strong>473 BEECH 200 406 MHz ELT installation Modification applicable on s/n BB616 and<br />
BB202 only.<br />
05.08.2005<br />
<strong>EASA</strong>.A.S.<strong>01</strong>6<strong>01</strong> FAIRCHILD SWEARINGEN SA ATC Mode S, ELT 406 MHz, Altimeter, Turn<br />
30.<strong>01</strong>.2006<br />
226-T(<br />
and Bank annunciator installation<br />
<strong>EASA</strong>.A.S.02930 FAIRCHILD SWEARINGEN SA Garmin GNS 530A VHF 8.33KHZ, Honeywell This STC is limited to the SA226 S/N T312 26.02.2007<br />
226<br />
KY 196B VHF 8.33 KHZ, BF Goodrich TAS<br />
SKY 899 Installation<br />
<strong>EASA</strong>.A.S.03<strong>01</strong>9 Installation of Avionic Upgrade according<br />
EMA/07/0<strong>01</strong>/SA226/VHF8.33-ATC-MFD-RDR<br />
30.<strong>04</strong>.2007<br />
10<strong>01</strong>4834 ELECTRONIQUE MAINTENANCE <strong>EASA</strong>.A.S.03050 BEECH 200 Installation of Garmin GTX330D Mode S<br />
21.<strong>04</strong>.2008<br />
AVIATION<br />
Transponder.<br />
10<strong>01</strong>5<strong>04</strong>5 ELECTRONIQUE MAINTENANCE <strong>EASA</strong>.A.S.03361 BEECH 200 Installation of new COM-NAV-GPS with AFM Supplement must be used when the<br />
<strong>04</strong>.08.2008<br />
AVIATION<br />
BRNAV capacity and coupled to AP.<br />
application is applied.Modification limited to sn<br />
BB616.<br />
10<strong>01</strong>7146 ELECTRONIQUE MAINTENANCE <strong>EASA</strong>.R.S.<strong>01</strong>249 EUROCOPTER FRANCE AS Installation of SAFE FLIGHT Power Line<br />
27.02.2007<br />
AVIATION<br />
355E<br />
Detector p/n 71<strong>01</strong>-5, in accordance with EMA<br />
EUROCOPTER FRANCE AS STC file n° 06/0<strong>01</strong>/AS355Serie/PLD revision 0,<br />
355F<br />
dated January 2006, or later <strong>EASA</strong> approved<br />
EUROCOPTER FRANCE AS<br />
355F1<br />
EUROCOPTER FRANCE AS<br />
355F2<br />
EUROCOPTER FRANCE AS<br />
355N<br />
revision.<br />
10<strong>01</strong>6097 ELISEN TECHNOLOGIES <strong>EASA</strong>.IM.A.S.02286 TCCA STC SA07-9 BOMBARDIER CL-600-2B19 Iridium Antenna Installation 31.05.2007<br />
10<strong>01</strong>6098 ELISEN TECHNOLOGIES <strong>EASA</strong>.IM.A.S.02287 TCCA STC SA07-3 BOMBARDIER CL-600-2B19 Aft Equipment Bay Steps 31.05.2007<br />
10<strong>01</strong>6099 ELISEN TECHNOLOGIES <strong>EASA</strong>.IM.A.S.02288 TCCA STC SA07-4 BOMBARDIER CL-600-2B19 Ladder Stowage 31.05.2007<br />
10<strong>01</strong>6100 ELISEN TECHNOLOGIES <strong>EASA</strong>.IM.A.S.02289 TCCA STC SA07-5 BOMBARDIER CL-600-2B19 Towbar Head Stowage 31.05.2007<br />
10<strong>01</strong>61<strong>01</strong> ELISEN TECHNOLOGIES <strong>EASA</strong>.IM.A.S.02290 TCCA STC SA07-6 BOMBARDIER CL-600-2B19 Main wheel stowage 31.05.2007<br />
10<strong>01</strong>6168 ELISEN TECHNOLOGIES <strong>EASA</strong>.IM.A.S.02395 TCCA STC SA07-20 BOMBARDIER CL-600-2B19 Miscellaneous Storage Box, Project No. 29R2-<br />
707<br />
03.07.2007<br />
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