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
10015799 ELECTRONIC CABLE SPECIALISTS, Inc. EASA.IM.A.S.01863 REV 1 FAA STC ST1193LA-T BOEING 767-300 SERIES Installation of Honeywell MCS-6000 SATCOM This installation must be installed in conjunction
08.03.2007
System
with Honeywell STC EASA.IM.A.S.02276 for
the installation of the SATCOM High-Gain
Antenna and Diplexer / Low Noise Amplifier
(D/LNA).
10015889 ELECTRONIC CABLE SPECIALISTS, Inc. EASA.IM.A.S.02008 FAA STC STC02075CH AIRBUS A300 MODEL B2-1A Installation of Universal Avionics Systems Aircraft Flight Manual Supplement ECS
20.09.2006
AIRBUS A300 MODEL B2-1C Corporation Terrain Awareness and warning 202604, revision B, dated 11 October 2005 or
AIRBUS A300 MODEL B2-203 System (TAWS)
later approved revisionInstruction for continued
AIRBUS A300 MODEL B2K-3C
airworthiness ECS 202604, revision B, dated 5
AIRBUS A300 MODEL B4-103
December 2005If the holder agrees to permit
AIRBUS A300 MODEL B4-203
AIRBUS A300 MODEL B4-2C
another person to use this certifi
10015992 ELECTRONIC CABLE SPECIALISTS, Inc. EASA.IM.A.S.02146 ST00694CH DC-9-81 (MD-81)
Installation of Dual Honeywell HT9100 GNSS 1. Limited to configuration III and IV.2.
21.05.2007
DC-9-82 (MD-82)
GPS Navigation System.
Compatibility of this design change with
DC-9-83 (MD-83)
previously approved modifications must be
DC-9-87 (MD-87)
determined by the installer.3. This STC is
approved only for the product configuration as
defined in the approved design d
10016069 ELECTRONIC CABLE SPECIALISTS, Inc. EASA.IM.A.S.02249 FAA STC ST02316CH DC-9-80 SERIES FAA STC ST02316CH - Elementary and Limited to configuration 3 of ECS MDL ECS-
28.02.2007
Enhanced Mode S.
203350 Rev. G dated July 7, 2006.This STC is
approved only for the product configuration as
defined in the approved design data referred to
in the paragraphs "Description" and
“Associated Technical Documentation”.
10016124 ELECTRONIC CABLE SPECIALISTS, Inc. EASA.IM.A.S.02317 FAA STC ST02303CH BOEING 767-200, -300 SERIES Installation of Enhanced Mode-S Transponder. The Airplane Flight Manual Supplement as
listed in Appendix A of Electronic Cable
Specialists Master Data List, Document No.
ECS-202463, Revision F, dated June 27,
2006, or later approved revision is required on
board the modified aircraft.
10016386 ELECTRONIC CABLE SPECIALISTS, Inc. EASA.IM.A.S.02714 FAA STC SA01527CH PILATUS PC-12
PILATUS PC-12/45
PILATUS PC-12/47
Installation of a Honeywell KMH 880 Multi-
Hazard Awareness System or a Honeywell
KTA 870 Traffic Advisory System.
10016388 ELECTRONIC CABLE SPECIALISTS, Inc. EASA.IM.A.S.02716 FAA STC ST01479CH BOEING 737-300-900 SERIES Installation of a Smiths Industries Flight
Management System Data Bus Portable
Computing Device Recorder.
10016507 ELECTRONIC CABLE SPECIALISTS, Inc. EASA.IM.A.S.02873 FAA STC ST02182CH BOEING 747-100
BOEING 747-200B
BOEING 747-200C
BOEING 747-200F
BOEING 747-300
BOEING 747-400
BOEING 747-400D
BOEING 747-400F
BOEING 747-SR
Installation of Elementary or Enhanced
Surveillance Mode S Transponder iaw
Electronic Cable Specialists Master Data List
ECS-202128, rev. AB, 7 January 2008 or later
approved revision.
Limitations as per Master Data List PC-12, PC-
12/45, PC-12/47, Installation of IHAS, ECS-
200836 Revision L, dated August 29, 2006, or
later FAA approved revision, Part III.
Limitations
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
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.
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14.06.2007
10.03.2008
17.07.2008
20.10.2008