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>6276 AIRCRAFT SYSTEMS AND<br />
<strong>EASA</strong>.IM.A.S.02565 FAA STC ST10268SC DC-9-80 (MD-80) SERIES FAA STC ST10268SC "installation of Universal 1. TGL 12 complied with.2. Prior to<br />
10.10.2007<br />
MANUFACTURING,<br />
Avionics Terrain Awareness Warning Ststem installation of this modification the installer must<br />
(TAWS)".<br />
determine that the interrelationship between<br />
this modification and any other previously<br />
installed modification will introduce no adverse<br />
effect upon the airworth<br />
10031221 AIRCRAFT SYSTEMS AND<br />
MANUFACTURING,<br />
FAA STC ST09<strong>04</strong>0SC B737-300, -400, -500 Installation of Digital Flight Data Recorder<br />
System (DFDR) using aTeledyne Digital Flight<br />
Data Acquisition Unit (DFDAU)<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 />
03.08.2<strong>01</strong>0<br />
10<strong>01</strong>6366 AIRCRAFT TECHNICAL DEVELOPMENT <strong>EASA</strong>.IM.A.S.02688 FAA STC ST02122LA AIRBUS A320 SERIES Installation of Aerocon Engineering Company<br />
14.03.2008<br />
Inc.<br />
(AEC) On-Board Airstair<br />
10<strong>01</strong>6409 AIRCRAFT TECHNICAL DEVELOPMENT <strong>EASA</strong>.IM.A.S.02741 REV. 3 FAA STC ST02112LA A318-111, -112, -121, -122 Installation of Cabin Interior Noise Reduction None. Prior to installation of this modification the 31.03.2<strong>01</strong>0<br />
Inc.<br />
A319-111, -112, -113, -114 Kit/Installation of new Thermal Insulation<br />
installer must determinethat the<br />
A319-115, -131, -132, -133 blankets in the cabinRevision of the <strong>EASA</strong> STC<br />
interrelationship between this modification<br />
<strong>EASA</strong>.IM.A.S.02741 to include A318-111/112/-<br />
and any otherpreviously installed<br />
121/-122 Models<br />
modification will introduce no adverse<br />
effect uponthe airworthiness of the<br />
product.The installatio<br />
10<strong>01</strong>6636 AIRCRAFT TECHNICAL DEVELOPMENT <strong>EASA</strong>.IM.A.S.03076 FAA STC ST<strong>01</strong>635 LA BOEING 737-700<br />
- Installation of Cabin Interior Noise 1. Prior to installation of this modification the<br />
20.<strong>01</strong>.2009<br />
Inc.<br />
BOEING 737-800<br />
Reduction Kit.- Validation of FAA<br />
installer must determine that the<br />
ST<strong>01</strong>635LA.<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.2.<br />
10<strong>01</strong>6645 AIRCRAFT TECHNICAL DEVELOPMENT <strong>EASA</strong>.IM.A.S.03088 FAA STC ST<strong>01</strong>568LA BOEING 737-700 - Installation of Cabin Interior Noise 1. Prior to installation of this modification the<br />
20.<strong>01</strong>.2009<br />
Inc.<br />
Reduction Kit.- Validation of FAA<br />
installer must determine that the<br />
ST<strong>01</strong>568LA.<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.2.<br />
10032264 AIRCRAFT TECHNICAL DEVELOPMENT<br />
FAA STC ST02317LA A330-200 Installation of Cabin Interior Noise Reduction Not applicable Prior to installation of this modification it 21.10.2<strong>01</strong>0<br />
Inc.<br />
Kit<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 />
10034009 AIRCRAFT TECHNICAL DEVELOPMENT<br />
Inc.<br />
10038108 AIRCRAFT TECHNICAL DEVELOPMENT<br />
Inc.<br />
10039327 AIRCRAFT TECHNICAL DEVELOPMENT<br />
Inc.<br />
FAA STC ST02112LA A320 Installation of Cabin Interior Noise Reduction<br />
Kit/Installation of new Thermal Insulation<br />
blankets in the cabin.<br />
FAA STC ST02382LA CL-600-2C10 Cabin Interior Noise Reduction Systems<br />
installation Kit in BombardierCL-600-2C10<br />
(Regional Jet Series 700, 7<strong>01</strong> & 702) Series<br />
Aircraft<br />
Not applicable 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 />
25.02.2<strong>01</strong>1<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 />
19.<strong>01</strong>.2<strong>01</strong>2<br />
REV. 1 FAA STC ST02361LA A340-311/-312/-313 Installation of On-Board Airstair Interaction of this STC with cabin arrangement Prior to installation of this modification it 24.07.2<strong>01</strong>2<br />
features has not beenevaluated.Should this must be determined thatthe<br />
STC be part of a cabin arrangement, the interrelationship between this modification<br />
interactions betweenthis STC and any cabin or and any other previouslyinstalled<br />
seating arrangements must be evaluated modification and/ or repair will introduce<br />
forcompliance with applicable certificati no adverse effectupon the airworthiness<br />
of the product.<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 64/<strong>462</strong>
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