04/01/2013 Page 1/462 - EASA

EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue
10015030 AVIONICS INTEGRATION &
EASA.A.S.03342 FOCA STC 34-45-004 CESSNA 525, CITIATION JET TCAS-400 & dual TDR-94D
10.10.2007
ENGINEERING
CESSNA 525A
installation.Change to the FOCA STC 34-45-
004 "TCAS-4000, Dual TDR-94D, GNS-430
Installation.By: Incorporation of an Gables
IST.G7614-() as an alternative ATC/TCAS
controller.
10015114 AVIONICS INTEGRATION &
ENGINEERING
EASA.A.S.03462 LEARJET 60 UNS-1B or 1C upgrade to UNS 1C+ 25.04.2008
10015143 AVIONICS INTEGRATION &
EASA.A.S.03503 1329-25 Upgraded Avionics systems:- UNS-1D to UNS- Reg.: HB-JGK S/N: 5233Valid for this S/N
14.07.2008
ENGINEERING
1D+ FMS- Dual VHF-20A system to VHF-22C only.
incl CTL-22C Control Head- Dual DME-42
system with 2 CTL-32C Control Head- Dual
VIR-30 NAV system with 2 CAD-31 Control
Adapter- Altimetry system with a IS&S Air Data
System
10015155 AVIONICS INTEGRATION &
EASA.A.S.03520 LEARJET 60 Installation of Iridium SAT/COM Antenna Installation of the Iridium SAT/COM antenna
22.04.2008
ENGINEERING
(Sensor Systems)
and the antenna coax outlet as covered by this
STC does not constitute an approval of the
utility system installation or operation.
10015213 AVIONICS INTEGRATION &
ENGINEERING
10015252 AVIONICS INTEGRATION &
ENGINEERING
10015260 AVIONICS INTEGRATION &
ENGINEERING
10015280 AVIONICS INTEGRATION &
ENGINEERING
10015292 AVIONICS INTEGRATION &
ENGINEERING
10017244 AVIONICS INTEGRATION &
ENGINEERING
10017268 AVIONICS INTEGRATION &
ENGINEERING
10028083 AVIONICS INTEGRATION &
ENGINEERING
10028084 AVIONICS INTEGRATION &
ENGINEERING
10028085 AVIONICS INTEGRATION &
ENGINEERING
10028086 AVIONICS INTEGRATION &
ENGINEERING
EASA.A.S.03628 LEARJET 31 P-RNAV Compliance Demonstration Prior to installation of this modification the
installer must determine that the
interrelationship between this modification and
any other previously installed modification will
introduce no adverse effect upon the
airworthiness of the product. The install
EASA.A.S.03697 BOMBARDIER CL-600-2B16 P-RNAV Compliance Prior to installation of this modification the
installer must determine that the
interrelationship between this modification and
any other previously installed modification will
introduce no adverse effect upon the
airworthiness of the product. The install
EASA.A.S.03718 REV 1 BEECH 390 Iridium SATCOM System Installation (Sky
Connect)
EASA.A.S.03806 REV. 2 CESSNA 206, 210 Installation of Aspen Avionics EFD 1000
system (STC to cover now CessnaC-206 &
newly added Cessna C-210 series)
This change is limited to the configuration of
aircraft / equipment type as listed under 3.1
Mechanical Installations”, in Engineering
Order, Doc. No. 788-062, Revision A, dated 13-
Jan-2009, or later approved revision.1 Prior
to installation of
Not valid if the Garmin 1000 ICS option is
installed.
25.08.2008
13.10.2008
09.02.2009
The approval holder shall fulfil the 25.06.2010
obligations of Part 21,
Paragraph21.A109. Prior to installation of
this modification it must be determined
thatthe interrelationship between this
modification and any other
previouslyinstalled modification and/ or
repai
20.04.2009
EASA.A.S.03834 CESSNA 206 SERIES Dual GNS 430w with TAS 600 SystemsBy Aspen EFD-1000 Primary Flight Display must
installing two GARMIN GNS430W with external be installed in the aircraft.
121.5MHz Frequency selection and an Avidyne
TAS 600 system
EASA.R.S.01441 A 109 K2 Replacement Euronav III by Euronav V Prerequisite conditions:- Dual GNS-530A
28.04.2008
(Euroavionics)By removing- the existing RN 5 installation- RN 5 Euronav III Map Generator
Euronav III Map Generatorand installing- a new installed with interface to the GNS-530A #2-
RN 6 Euronav V Digital Map Generator CLN.14-3.0 Control Unit installed- DYNT64-2.0
Display installed
EASA.R.S.01488 EC-135-T2 COM/NAV/ATC Avionics System Installation. 1. Prior to installation of this modification the
installer must determine that the
interrelationship between this modification and
any other previously installed modification will
introduce no adverse effect upon the
airworthiness of the product.2.
04.02.2009
P-EASA.A.S.03930 LEARJET 35A Installation of Artex ELT C406-02 (Cobham). None. None. 01.12.2009
P-EASA.A.S.03936 LEARJET 35A Installation of ART 2000 Weather Radar with
KMD 850 MFD (Honeywell).
None. None. 01.12.2009
P-EASA.A.S.03933 LEARJET 35A Installation of SSFDR F1000 (L-3
Communications).
None. None. 01.12.2009
P-EASA.A.S.03932 LEARJET 35A Installation of EGPWS Mk VIII (Honeywell). None. None. 01.12.2009
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