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>6252 ELLIOTT AVIATION <strong>EASA</strong>.IM.A.S.02529 FAA STC SA02447CH BEECH 200<br />
Installation of a Rockwell Collins IFIS-5000<br />
27.02.2008<br />
BEECH 200C<br />
BEECH 200CT<br />
BEECH 200T<br />
BEECH 300<br />
BEECH 300C<br />
Integrated Flight Information system.<br />
10<strong>01</strong>6254 ELLIOTT AVIATION <strong>EASA</strong>.IM.A.S.02532 FAA STC ST02431CH FALCON 10 <strong>EASA</strong> Validation of FAA STC<br />
The aircraft must be equipped with Universal<br />
13.05.2008<br />
ST02431CH<strong>EASA</strong> Validation is limited to Avionics EFI-890R Electronic Flight Instrument<br />
Provisions for Installation of a Universal System (EFIS) as installed by Elliott Aviation’s<br />
Avionics Application Server Unit (ASU) on STC <strong>EASA</strong>.IM.A.S.<strong>01</strong>713.This <strong>EASA</strong> Approval<br />
Falcon 10<br />
is limited to provisions for installation only with<br />
the ASU System deactiv<br />
10<strong>01</strong>6474 ELLIOTT AVIATION <strong>EASA</strong>.IM.A.S.02822 FAA STC ST02548CH FALCON 10 <strong>EASA</strong> Validation of FAA STC<br />
ST02548CHInstallation of an International<br />
Communications Group ICS-120 Iridium<br />
Satellite Telephone System<br />
Prior to installation of this modification the<br />
installer must determine that the<br />
interrelationship between this modification and<br />
any other previously installed modification will<br />
introduce no adverse effect upon the<br />
airworthiness of the product. The install<br />
10<strong>01</strong>6475 ELLIOTT AVIATION <strong>EASA</strong>.IM.A.S.02823 FAA STC ST02547CH FALCON 10 <strong>EASA</strong> Validation of FAA STC<br />
Prior to installation of this modification the<br />
ST02547CHInstallation of a Universal Avionics installer must determine that the<br />
Systems Corporation UL-7<strong>01</strong> UniLink System interrelationship between this modification and<br />
any other previously installed modification will<br />
introduce no adverse effect upon the<br />
airworthiness of the product. The install<br />
10029872 ELLIOTT AVIATION FAA STC STC02784CH BEECHJET 400/400A Installation of Honeywell Digital Flight Data None Prior to installation of this modification it 28.<strong>04</strong>.2<strong>01</strong>0<br />
RecorderValidation of FAA STC STC02784CH<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 />
10029873 ELLIOTT AVIATION FAA STC STC02783CH BEECHJET 400 Installation of an Artex C406-2 Emergency<br />
Locator Transmitter (ELT)Validation of FAA<br />
STC STC02783CH<br />
10<strong>01</strong>5890 EMBRAER - EMPRESA BRASILEIRA <strong>EASA</strong>.IM.A.S.02009 CTA STC2006S02-09 EMBRAER EMB-135BJ CTA STC2006S02-09 "Installation of a 30' 1. Limited to EMB-135BJ SN 145000802.<br />
LCD monitor and Playstation Entertainment Instructions for Continued Airworthiness Report<br />
System iaw Avionic Services master drawing No. 135-23-0008 Rev. 0 dtd. 9. Sep. 05 or<br />
list 135-23-0<strong>01</strong> Rev. D dtd. 28. Nov. 05 or later later accepted revision.2. This STC is<br />
approved revision<br />
approved only for the product configuration as<br />
defined in the approved design data<br />
10027373 EMBRAER - EMPRESA BRASILEIRA P-<br />
<strong>EASA</strong>.IM.A.S.03273<br />
ANAC STC 2009S05-14 EMB-500 Installation of a Honeywell HF Communications<br />
System, Model KHF-1050 andoptionally the<br />
Avtech Corporation SELCAL decoder, Model<br />
CSD-714.<br />
10038234 EMBRAER GPX Ltda. (PC 722) REV. 1 EMB-135BJ/LR/ER<br />
<strong>EASA</strong> Validation of ANAC STC 2<strong>01</strong>0S10-18.<br />
EMB-145<br />
Electronic Flight Bag<br />
EMB-145ER/EU/EP/MP/LR/LU/MK (EFB)Installation.Description as<br />
per:ESCMSC002-Rev A, dated 17th January<br />
2<strong>01</strong>2.Master Documents List ESCCCD003-<br />
Rev B, dated 17th January 2<strong>01</strong>2.<br />
10038291 EMBRAER GPX Ltda. (PC 722) EMB-135BJ <strong>EASA</strong> validation of ANAC STC N°2<strong>01</strong>1S09-<br />
02Installation of a cabinet and a 17'' video<br />
monitor on EMB-135BJ aircraft<br />
26.05.2008<br />
26.05.2008<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 />
28.<strong>04</strong>.2<strong>01</strong>0<br />
Required Markings and Placards:-.In close<br />
proximity to the 5A breaker in panel LH circuit<br />
breaker "HFPWR". In close proximity to the<br />
30A breaker in circuit breaker of LPDU<br />
"HFAMPL". (If applicable) In close proximity to<br />
the 5A breaker in panel LH circuitbr<br />
Prior to installation of this modification the<br />
installer must determinethat the<br />
interrelationship between this modification<br />
and any otherpreviously installed<br />
modification will introduce no adverse<br />
effect uponthe airworthiness of the<br />
23.<strong>01</strong>.2007<br />
25.09.2009<br />
None<br />
product.The installatio<br />
None <strong>01</strong>.02.2<strong>01</strong>2<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 />
03.02.2<strong>01</strong>2<br />
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