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 />
10034165 AEROCONSEIL F2000 FALCON 2000 S/N 226 INTERIOR<br />
Restricted to S/N 226 Prior to installation of this modification it 14.03.2<strong>01</strong>1<br />
MATERIAL CHANGESChange consists in<br />
must be determined thatthe<br />
refurbishing certain panels- Windows Panels &<br />
interrelationship between this modification<br />
Valance Panels (lower and upper)- Glass<br />
and any other previouslyinstalled<br />
Carbon 250/56%/G874 panels.<br />
modification and/ or repair will introduce<br />
no adverse effectupon the airworthiness<br />
of the product<br />
10034950 AEROCONSEIL AS 365N3 Installation of structural provisions (floor fittings)<br />
for cabin layoutModification in accordance with<br />
AEROCONSEIL Installation ServiceBulletin<br />
2<strong>01</strong>8-<strong>01</strong>-A-31<strong>01</strong>.<br />
10035182 AEROCONSEIL A300 B4-6<strong>01</strong>, A300 B4-603,<br />
A300 B4-620, A300 B4-622,<br />
A300 B4-622 R, A300 B4-605 R,<br />
A300 C4-605 R VARIANT F,<br />
A300 C4-620,<br />
A300 F4-605 R, A300 F4-622 R<br />
10035880 AEROCONSEIL B777-200, B777-200LR<br />
B777-300, B777-300ER<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 />
16.05.2<strong>01</strong>1<br />
Aeroconseil STC <strong>04</strong>90-1 Aircell ST3100 None. Prior to installation of this modification it <strong>01</strong>.06.2<strong>01</strong>1<br />
SATCOM Installation on A300-600s.This STC<br />
must be determined thatthe<br />
covers the installation of a Satellite Telephone<br />
interrelationship between this modification<br />
SystemTransceiver, a Telephone adapter with<br />
and any other previouslyinstalled<br />
Display, a Base cradle for theCordless Handset<br />
modification and/ or repair will introduce<br />
and a Satellite antenna in accordanc<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
0555-<strong>01</strong>: Provisions of OnAir GSM/Internet<br />
System on B777<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 />
25.07.2<strong>01</strong>1<br />
10036272 AEROCONSEIL REV. 1 A340-311/-312/-313 A340 Cabin Reconfiguration & Zodiac SiT In- 1. Aeroconseil Modification, ref: MOD 7<strong>04</strong>9-<strong>01</strong>, Prior to installation of this modification it 09.08.2<strong>01</strong>2<br />
Flight EntertainmentInstallation The<br />
must be installed,being a pre-requisite to must be determined thatthe<br />
modification consists in reconfiguring the A340 this STC.2. This STC is limited to the A340- interrelationship between this modification<br />
cabin compartment byreplacing the economy 300 MSNs 197 and 378<br />
and any other previouslyinstalled<br />
class seats, from 218 Y/C seats to 215 Y/C<br />
modification and/ or repair will introduce<br />
seatswith Sicma 3537 series seats, and inst<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
10037524 AEROCONSEIL A330-3<strong>01</strong>/-302/-303<br />
A330-321/-322/-323<br />
A330-341/-342/-343<br />
Panasonic eXPhone System activation on<br />
A330-300 with eX2 IFEThis STC installs a<br />
Panasonic eXphone System allowing, in<br />
conjunctionwith other devices, the use of<br />
cellphones during flight.<br />
10037893 AEROCONSEIL 747-100, -200, -200F Installation of a CAS-81 TCAS II system and<br />
Dual TRA-67 "Mode S"transponders in<br />
accordance with Aeroconseil Master Drawing<br />
List0520-<strong>01</strong>-A-2103-R00 or later approved<br />
revisions.<br />
10038574 AEROCONSEIL A330-200, -300 A330 Tape Video Reproducer Unit Installation<br />
The change consist in areplacement of each<br />
MAS Video Tape Player (VTP) by new digital<br />
videoreproducer units manufactured by<br />
Goodrich installed in the aircraftexisting Video<br />
10038663 AEROCONSEIL REV. 1 777-200, 777-200LR<br />
777-300, 777-300ER<br />
Contro Center.<br />
<strong>04</strong>11-<strong>01</strong>: Installation/activation of OnAir<br />
GSM/Internet System on B777<br />
The following modifications are prerequisites to Prior to installation of this modification it 02.12.2<strong>01</strong>1<br />
the installation ofthis STC:-Airbus Minor must be determined thatthe<br />
Change ref: 20<strong>01</strong>90 - Approved under Airbus interrelationship between this modification<br />
DOA<strong>EASA</strong>.21J.031, on 22 February 2<strong>01</strong>1- and any other previouslyinstalled<br />
Delta Engineering STC ref: ODA-2234-<strong>01</strong> - modification and/ or repair will introduce<br />
<strong>EASA</strong> Approval 10036548 Rev 1or later revisio no adverse effectupon the airworthiness<br />
of the product.<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 />
<strong>04</strong>.<strong>01</strong>.2<strong>01</strong>2<br />
this change is limited to A330-200 and A330-<br />
300, providing that the VCCP/N RDAA902251<br />
isinstalled, and still in the configuration<br />
approved by the aircraftmanufacturer (no other<br />
STCs modifying the VCC before this change).<br />
None 27.02.2<strong>01</strong>2<br />
Per AFM Supplement <strong>04</strong>11-<strong>01</strong>-AThis<br />
modification is limited as stated below except<br />
similaritydemonstrated per Document 00<strong>01</strong>-<strong>01</strong>-<br />
B-0914 (Classification of ModificationChange<br />
Procedure for Connectivity System).STC<br />
effectivity: Boeing 777-300ER MSN 33377,<br />
34568,<br />
To be installed concurrent with <strong>EASA</strong><br />
STC 10035880 (Provisions)Prior to<br />
installation of this modification it must be<br />
determined thatthe interrelationship<br />
between this modification and any other<br />
previouslyinstalled modification and/ or<br />
repair will introduce<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 17/<strong>462</strong><br />
08.03.2<strong>01</strong>2
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