04/01/2013 Page 1/462 - EASA
04/01/2013 Page 1/462 - EASA
04/01/2013 Page 1/462 - EASA
You also want an ePaper? Increase the reach of your titles
YUMPU automatically turns print PDFs into web optimized ePapers that Google loves.
<strong>EASA</strong> STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue<br />
10038251 DELTA ENGINEERING CORPORATION FAA STC ST02890NY-D A319 Installation of Panasonic Global<br />
None Prior to installation of this modification it <strong>01</strong>.02.2<strong>01</strong>2<br />
Communication System Antenna<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 />
10038944 DELTA ENGINEERING CORPORATION FAA STC ST02889NY-D A330-2<strong>01</strong>, -202, -203<br />
A330-223, -243<br />
Panasonic Global Communication System -<br />
System installation This STC installs of<br />
Panasonic Global Communication System<br />
(GCS) andactivate the wireless portion.<br />
10<strong>04</strong><strong>01</strong>02 DELTA ENGINEERING CORPORATION REV. 1 FAA STC ST02903NY-D B747-400 Installation of Panasonic eX2 In-Flight<br />
Entertainment system witheXPhone in<br />
accordance with Delta Engineering Master<br />
Data list<strong>01</strong>07-07608-2280 Rev. E, dated<br />
September 13, 2<strong>01</strong>2 or later FAA<br />
approvedrevisions.Validation of FAA STC<br />
ST02903NY-D.<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 />
23.03.2<strong>01</strong>2<br />
The Panasonic eXPhone system must The Instructions for Continued<br />
30.10.2<strong>01</strong>2<br />
interface with the following<br />
Airworthiness, Electrical<br />
existingsystems/components which must be WiringInterconnect System Instructions<br />
installed in a manner acceptable to<br />
for Continued Airworthiness andAirplane<br />
theauthorities. The below listed required Flight Manual Supplement as listed on<br />
existing systems are not approvedby this STC. the Master Data List arerequired with this<br />
Required Supplemental Type C<br />
installation. Prior to installation of<br />
10<strong>04</strong>0214 DELTA ENGINEERING CORPORATION FAA STC ST029<strong>01</strong>NY-D B747-400 Installation of a Panasonic eX2 In-Flight None The Instructions for Continued<br />
18.06.2<strong>01</strong>2<br />
Entertainment System inaccordance with Delta<br />
Airworthiness and Electrical<br />
Engineering Master Data List <strong>01</strong>07-07459-<br />
WiringInterconnect System Instructions<br />
2283Revision B, dated May 9, 2<strong>01</strong>2 or later<br />
for Continued Airworthiness as listedon<br />
FAA approved revisionsValidation of FAA STC<br />
the Master Data List are required with this<br />
ST029<strong>01</strong>NY-D<br />
installation.FAA STC ST02227SE, <strong>EASA</strong><br />
approval 10039535, must be installed<br />
10<strong>04</strong>1776 DELTA ENGINEERING CORPORATION FAA STC ST02714NY-D 737-600, 737-700, 737-700C,<br />
737-800, 737-900, 737-900ER<br />
Installation of provisions for dual NavAero<br />
Electronic Flight Bags withNavaero Mount.<br />
10<strong>04</strong>2191 DELTA ENGINEERING CORPORATION FAA STC ST02<strong>04</strong>9NY B747-400 Installation of Panasonic Avionics Corporation<br />
System 3000i PassengerEntertainment System<br />
in accordance with Delta Engineering Master<br />
DrawingList <strong>01</strong>07-05381-2073, Revision D,<br />
dated June 08, 2005 or later approvedrevision.<br />
Validation of FAA STC ST02<strong>04</strong>9NY.<br />
10<strong>04</strong>2528 DELTA ENGINEERING CORPORATION FAA STC ST003056CH 737-800 Validation of FAA STC ST003056CH:<br />
Installation of Panasonic<br />
GlobalCommunications suite (GCS) System<br />
Provisions in accordance withArmstrong<br />
Aerospace Master Data List DC1<strong>04</strong>-9<strong>04</strong>1-00,<br />
Revision B, dated 22September 2<strong>01</strong>1.Revision<br />
1: Transfer of STC from Armstro<br />
10<strong>04</strong>2791 DELTA ENGINEERING CORPORATION FAA ST02926NY-D A330-2<strong>01</strong>, A330-202<br />
A330-203, A330-223<br />
A330-243<br />
10<strong>01</strong>5483 DEVORE AVIATION CORPORATION OF <strong>EASA</strong>.IM.A.S.<strong>01</strong>243 FAA STC ST09191AC BOEING 737-200<br />
BOEING 737-200C<br />
BOEING 737-300<br />
BOEING 737-400<br />
BOEING 737-500<br />
Provisions for Panasonic Global<br />
Communication System: This project covers<br />
the installation and deactivation of a<br />
PanasonicGlobal Communication Suite (GCS)<br />
and Cell Modem on Airbus A330-200.<br />
Theactivation of the equipment installed is not<br />
cover by this proj<br />
InInstallation of DeVore Wing Forward Position<br />
Light Assembly according to FAA STC<br />
ST09191AC<br />
Only for Installation of NavAero Mount<br />
("Configuration 2").The installation of ECS<br />
Mount ("Configuration 1") is not certified.<br />
Prior to installation of this modification it 15.10.2<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 theairworthiness<br />
of the product.<br />
None. STC ST<strong>01</strong>492SE is required to be<br />
installed as a prerequisite<br />
foraccomplishing this STC. The<br />
Instructions for Continued Airworthiness<br />
as listed on the MasterData List are<br />
required with this installation. Prior to<br />
installation of this modification it must be<br />
1) The Panasonic Global Communication Suite<br />
System for which theseprovisions are installed<br />
and these provisions activated in<br />
accordancewith a separate STC, <strong>EASA</strong> STC<br />
10038436.2) The aircraft operator must<br />
perform the instructions for<br />
continuedairworthiness<br />
This approval does not cover the activation of<br />
the components installed.The wiring related to<br />
this modification must not be connected and<br />
mustbe properly stowed in order to assure that<br />
the equipment installed isnot energized.<br />
1. According to Limitations Section of FAA<br />
STC ST09191AC2. This STC is approved only<br />
for the product configuration as defined in the<br />
approved design data referred to in the<br />
paragraph "Description". Compatibility with<br />
other aircraft/engine configurations sh<br />
14.11.2<strong>01</strong>2<br />
Prior to installation of this STC it must be 07.12.2<strong>01</strong>2<br />
determined that theinterrelationship<br />
between this STC and any other<br />
previously installedSTC, modification and<br />
/ or repair will introduce no adverse effect<br />
uponthe airworthiness of the product.<br />
Prior to installation of this modification it 18.12.2<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 />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 186/<strong>462</strong><br />
25.10.2005
Change language