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
10041959 APICAL INDUSTRIES, Inc. FAA STC NO. SR02425LA A119, A119 MK II EASA Validation of FAA STC No. SR02425LA None. Prior to installation of this modification it 26.10.2012
"Installation of ApicalIndustries, Inc. Cable
must be determined thatthe
Cutter Kit".
interrelationship between this modification
and any other previouslyinstalled
modification and/ or repair will introduce
no adverse effectupon the airworthiness
of the product.
10042766 APICAL INDUSTRIES, Inc. FAA STC SR02373LA EC130B4 Installation of Fresh Air Vents in accordance
with Apical Industries,Inc. Master Document
List MD130-3. This STC is the validation of
FAA STC SR02373LA (date of
issuanceSeptember 12, 2012).
10016824 APOLLO SPRAY SYSTEMS EASA.IM.R.S.01194 SR01215CH ROBINSON R44 Installation of Apollo Spray system DTM-4
agricultural sprayer onto Robinson R44
helicopter. EASA validation of FAA STC
SR01215CH
10042428 APPAREO SYSTEMS, L.L.C. FAA STC SR02797CH AS350B1, AS350B2,
AS350B3, AS350BA.
10015635 ARC AVIONICS CORP. EASA.IM.A.S.01591 FAA STC ST02959AT BOEING 737-300 SERIES
BOEING 737-400 SERIES
BOEING 737-500 SERIES
10015665 ARC AVIONICS CORP. EASA.IM.A.S.01641 FAA STC SA2890AT FAIRCHILD SWEARINGEN SA
226
FAIRCHILD SWEARINGEN SA
227
10016083 ARC AVIONICS CORP. EASA.IM.A.S.02267 FAA STC03354AT BOEING 737-200
BOEING 737-300
10016084 ARC AVIONICS CORP. EASA.IM.A.S.02269 FAA ST03356AT BOEING 737-200
BOEING 737-300
10016085 ARC AVIONICS CORP. EASA.IM.A.S.02270 REV. 2 FAA ST03362AT BOEING 737-200
BOEING 737-300
10016086 ARC AVIONICS CORP. EASA.IM.A.S.02271 FAA STC ST03363AT BOEING 737-200
BOEING 737-300
10016298 ARC AVIONICS CORP. EASA.IM.A.S.02595 FAA STC ST03458AT BOEING 737-300
BOEING 737-400
BOEING 737-500
Installation of Vision 1000 System in
accordance with Vision 1000 MasterDocument
List 606586-000011This STC is the validation
of FAA STC SR02797CH (date of
issuanceDecember 28, 2009)
Installation of Collins Model 700 High
Frequency (HF) Communication System and
HF Antenna
None. Prior to installation of this modification it
must be determined thatthe
interrelationship between this modification
and any other previouslyinstalled
modification and/ or repair will introduce
no adverse effectupon the airworthiness
of the product.
18.12.2012
Certified in restricted category.All limitations of
RFM supplement apply.
None If the holder agrees to permit another
person to use this certificate tomodify the
product, the holder shall give to the other
person writtenevidence of that
permission.Prior to installation of this
modification it must be determined
Installation of a Honeywell Model CAS 67A Prior to installation of this modification the
Traffic Alert and Collision Avoidance System II installer must determine that the
(TCAS II) with Single Mode-S Transponder interrelationship between this modification and
MST 67A iaw FAA STC SA02890AT. any other previously installed modification will
FAIRCHILD SWEARINGEN SA 26
introduce no adverse effect upon the
airworthiness of the product. The install
Installation of a single Universal Avionics Class
“A” TAWS system on 737-300 series aircraft.
12.02.2007
30.11.2012
thatthe interrelations
According to FAA STC ST02959AT 17.11.2005
The aircraft has to be equipped with a
Universal EFIS to display the TAWS terrain.
EASA Approved Flight Manual Supplement
ARC Avionics document 730-061505 Rev A
for Boeing 737-300 series aircraft, dated Feb 8
2007 is a part of this STC.
Installation of a dual Universal Avionics UNS- The aircraft have to be equipped with a
1F FMS sys on Boeing 737-300 aircraft Universal Avionics EFIS as it provides the
Installation includes 2 Nav Control Units Navigation Displays and Data Concentrator
(NCU)in the EE bay and 2 GPS antennas. Units M integrate the aircraft sensors and
Center pedestal pilot and co-pilot Control communications. FAA Approved Flight Manual
Display Units (CDU). Nav data can be selected Supplement, ARC Avionics document 730an
120605
Installation of a dual Universal Avionics UNS-
1F Flight ManagementSystem (FMS) or UNS-
1Fw WAAS capabe FMS, on- Boeing 737-200
and 737-300 aircraft without EFIS
(Configuration I)- Boeing 737-300 aircraft with
original Honeywell or Collins
EFIS(Configuration
Installation of a single Universal Avionics Class
“A” TAWS system on 737-200 series aircraft.
none Prior to installation of this modification it
must be determined thatthe
interrelationship between this modification
and any other previouslyinstalled
modification and/ or repair will introduce
no adverse effectupon the airworthiness
of the product.
The aircraft has to be equipped with a
Universal EFIS to display in the center pedestal
in order to display the TAWS terrain. This MFD
can be part of this installation, or pre-existing
as the 737-200 series Aircraft. EASA
Approved Flight manual Supplement
Installation upgrade to replace the existing - AFM Document, ARC Avionics Document
system with either Honeywell or Collins Dual 730-030806, for Boeing 737-300, -400, -500
Enhanced Mode S Transponder system. The series aircraft, dated 2 July 2007, or later
existing Omni directional antenna is compatible EASA approved revision.
with the new system and will not be replaced.
The two Honeywell TRA-67A or Col
04/01/2013 Page 80/462
05.09.2008
03.07.2007
31.05.2007
28.04.2011
27.06.2007
10.01.2008