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 />
100321<strong>04</strong> JAMCO AMERICA INC FAA STC ST<strong>01</strong>094SE 747-400 Installation of an interior reconfiguration of the None STC ST<strong>01</strong>482NY, <strong>EASA</strong>.A.S.03195, 07.10.2<strong>01</strong>0<br />
main and upper decksin 747-400 airplanes in<br />
(IFE system, purser work station,<br />
accordance with Jamco America, Inc.<br />
videomonitors and projectors) and STC<br />
MasterDrawing List no. IA-072MDL, Revision<br />
ST<strong>01</strong>519NY,<br />
AD dated 19 September 2008 or laterapproved<br />
<strong>EASA</strong>.IM.A.S.03197,(Installation of Inrevision<br />
Validation of FAA STC ST<strong>01</strong>094<br />
Seat Power Supply) must be installed<br />
concurrentlywith this STC.Prior to<br />
installation of this modificatio<br />
10<strong>04</strong>1373 JAMCO AMERICA INC FAA STC ST02107SE-D B777-300 Validation of FAA STC ST02107SE-D related Approval of this change in type design is STC ST03928AT-D, Installation of an IFE 11.09.2<strong>01</strong>2<br />
to Interior Reconfiguration.<br />
applicable to the above modelaircraft only. system and components, must<br />
beinstalled concurrently with this<br />
modification. STC ST03684AT,<br />
Installation of a photo luminescent floor<br />
proximitylighting system, as amended for<br />
the Boeing Model 777-300 seriesaircraft,<br />
10<strong>04</strong>1806 JAMCO AMERICA INC FAA STC ST<strong>01</strong>884SE-D 747-400 Installation of a galley modification on Boeing<br />
747-400 series aircraftin accordance with<br />
Jamco America, Inc. Master Drawing List<br />
(MDL) 1419-1,Rev.E, dated May 25, 2<strong>01</strong>2, or<br />
later FAA approved revision.Validation of FAA<br />
STC ST<strong>01</strong>884SE-D<br />
10<strong>04</strong>2094 JAMCO AMERICA INC FAA STC ST<strong>01</strong>514SE B747-400 Lavatory and galley modification of 747-400<br />
series airplanes inaccordance with Jamco<br />
America, Inc. Master Data List IA-102MDL,<br />
Rev. D,dated March 15,2005, or later FAA<br />
approved revision. Validation of FAA STC<br />
ST<strong>01</strong>514SE.<br />
10<strong>01</strong>6454 JAZZ AVIATION LP <strong>EASA</strong>.IM.A.S.02800 TC STC SA03-70 BOMBARDIER DHC-8-100<br />
SERIES<br />
BOMBARDIER DHC-8-200<br />
SERIES<br />
BOMBARDIER DHC-8-300<br />
SERIES<br />
10033847 JCB AERO SA A320 Installation of Hi-Low Table for VIP cabin<br />
interior<br />
10<strong>01</strong>6<strong>01</strong>0 JCM AERODESIGN LIMITED <strong>EASA</strong>.IM.A.S.02175 O-LSA06-268/D ISSUE 1 BOMBARDIER DHC-8-311 EMS Installation as per TCCA Limited<br />
Supplemental Type Certificate # O-LSA06<br />
268/D, Issue 1, dated 13 September 2006<br />
10<strong>01</strong>6783 JCM AERODESIGN LIMITED <strong>EASA</strong>.IM.R.S.<strong>01</strong>124 REV. 2 TCCA STC SH02-2 EUROCOPTER FRANCE AS 350<br />
B3<br />
S/N 29262 None 17.10.2<strong>01</strong>2<br />
FAA STC ST<strong>01</strong>492SE, interior reconfiguration<br />
of passenger seating, mustbe installed<br />
concurrently with this STC.<br />
Cockpit Door Electronic Strike System. 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.This AFM Sup<br />
Installation of Optech Inc. Airborne Laser<br />
Terrain Mapper ALTM 1225 or ALTM 3033 in<br />
Eurocopter AS 350B1 and AS 350B2 rotorcraft<br />
(approved under <strong>EASA</strong>.IM.R.S.<strong>01</strong>124 – initial<br />
issue).Installation of Optech Inc. Airborne Laser<br />
Terrain Mapper ALTM 3100 in Euroco<br />
10<strong>01</strong>5264 JET AVIATION AG <strong>EASA</strong>.A.S.03726 REV. 1 GULFSTREAM V Iridium Antenna InstallationA dual Iridium<br />
antenna has been installed on top of the<br />
fuselage located between Sta. 539.5 & Sta.<br />
554.5.<br />
10<strong>01</strong>5626 JET AVIATION AG <strong>EASA</strong>.IM.A.S.<strong>01</strong>578 REV. 2 BOMBARDIER CL-600-1A11 (CL-<br />
600<br />
BOMBARDIER CL-600-2A12 (CL-<br />
6<strong>01</strong><br />
BOMBARDIER CL-600-2B16<br />
Prior to installation of this modification it 07.11.2<strong>01</strong>2<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 />
30.06.2008<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 />
14.02.2<strong>01</strong>1<br />
DHC-8-311, S/N. 216 20.12.2006<br />
1. This STC is not approved for AS350 B3<br />
aircraft when equipped with Eurocopter Mod<br />
OP-3369 (2370 kg certified weight<br />
extension).2. Prior to installation of this<br />
modification the installer must determine that<br />
the interrelationship between this modifi<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<br />
will introduce no adverse effect upon the<br />
airworthiness of the product.<br />
22.05.2008<br />
19.12.2008<br />
Activation of RAAS 13.<strong>01</strong>.2009<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 284/<strong>462</strong>
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