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 />
10035106 HEATH TECNA, INC. FAA STC ST02072SE A330-2<strong>01</strong>, A330-202, A330-203 Installation of New J Class Crew Rest for none Prior to installation of this modification it 26.05.2<strong>01</strong>1<br />
A330-223, A330-243<br />
Qantas Airlines A330-200seriesThis STC<br />
must be determined thatthe<br />
installs a removable crew rest curtain and<br />
interrelationship between this modification<br />
curtain header<br />
and any other previouslyinstalled<br />
modification and/ or repair will introduce<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
10039535 HEATH TECNA, INC. FAA ST02227SE 747-400 Installation of 2 new avionics racks in the EE Approval of this change applies to Boeing 747- Instructions for Continued Airworthiness<br />
bay of a Boeing 747-400series aircraft in 400 aircraft listed inHPD-DL-162 Rev.A, dated Heath Tecna Inc. Doc HTM<br />
accordance with Heath Tecna Inc. Master Data April 12, 2<strong>01</strong>2 or later approved revisions only 10<strong>04</strong>,Revision B, dated April 4, 2<strong>01</strong>2<br />
ListHPD-DL-162 Rev. A, dated April 12, 2<strong>01</strong>2<br />
must be incorporated into the<br />
or later approved revision.<br />
operatorsmaintenance program. Prior to<br />
installation of this modification it must be<br />
determined thatthe interrelationship be<br />
10<strong>01</strong>4<strong>04</strong>0 HEATHTECNA <strong>EASA</strong>.A.S.<strong>01</strong>114 B767-300 SERIES Introduction of Stowage 4B and infill panel to<br />
British Airways aircraft as defined in the<br />
modification definition document and<br />
Declaration of Design and Performance (DDP)<br />
10<strong>01</strong>4078 HEATHTECNA <strong>EASA</strong>.A.S.<strong>01</strong>170 B747-400 Reconfiguration of Cabin Interior from current<br />
387SIA passenger cabin configuration<br />
(16F+58B+313Y for RT 514) to a 383<br />
(12F+47B+324Y), Cathy Pacific Boing 747-400<br />
fleet standard passenger cabin configuration.<br />
10<strong>01</strong>4143 HEATHTECNA <strong>EASA</strong>.A.S.<strong>01</strong>261 B747-400 SN 25127 & 25128 Heath Techna Modification C943 - Cathay<br />
Interiors Modification.<br />
10<strong>01</strong>4298 HEATHTECNA <strong>EASA</strong>.A.S.<strong>01</strong>542 B767-300 Business Class Footstool Assemblies on British<br />
Airways Boeing 767-300<br />
As defined in DDP, Aircraft Serial MSN 26548.<br />
Zero Occupancy. For this modification to be<br />
accepted on an EU registered aircraft, requires<br />
the operator to confirm that all the associate<br />
FAA and Hong Kong CDA modifications have<br />
been <strong>EASA</strong> approved.<br />
1. As defined in DDP Aircraft Serial Numbers<br />
25172 & 25128.2. Zero Occupancy.3. For this<br />
modification to be accepted on an EU<br />
registered aircraft requires the operator to<br />
confirm that all the associated FAA &Hong<br />
King CAD modifications have been <strong>EASA</strong><br />
appro<br />
This STC is limited to S/N 24340, 24341,<br />
252<strong>04</strong>, 25444, 25442, 25732, 25826, 25828,<br />
25829, 27140, 24335, 24336, 25831 and<br />
10<strong>01</strong>4519 HEATHTECNA <strong>EASA</strong>.A.S.02600 REV 1 B747-400 Cathay Pacific B747 Cabin Re-Configuration<br />
25834.<br />
1. Restricted to MSN 27132, MSN 27069 &<br />
07.<strong>04</strong>.2008<br />
REV 1<br />
MSN 265522. Zero occupancy3. This STC is<br />
approved only for the product configuration as<br />
defined in the approved design data referred to<br />
in the paragraphs "Description" and<br />
"Associated Technical Documentation".<br />
Compat<br />
10<strong>01</strong>4998 HEATHTECNA <strong>EASA</strong>.A.S.03298 DC-9 SERIES Meridiana DC-9 Series Stow Bin Extension. Restricted to ASN 49247,49248, 49531,<br />
49669, 49740, 499<strong>01</strong>, 49902, 49903, 53064,<br />
49808, 53182, 49785, 49792, 49935, 49951,<br />
49854, 53<strong>01</strong>3.<br />
20.11.2007<br />
10<strong>01</strong>6868 HELICOPTER TECHNOLOGY COMPANY <strong>EASA</strong>.IM.R.S.<strong>01</strong>244 FAA STC SR<strong>01</strong>282LA MD HELICOPTERS 369A Installation of a Tail Rotor Blade Assembly. N/A 15.03.2007<br />
MD HELICOPTERS 369D<br />
MD HELICOPTERS 369E<br />
MD HELICOPTERS 369FF<br />
MD HELICOPTERS 369H<br />
MD HELICOPTERS 369HE<br />
MD HELICOPTERS 369HM<br />
MD HELICOPTERS 369HS<br />
(STC Classified as Basic by the FAA).<br />
10<strong>01</strong>5311 HELICOPTERES GUIMBAL <strong>EASA</strong>.E.S.<strong>01</strong>0<strong>01</strong> REV. 1 O-360-J2A Low Temperature Extension - STC<br />
None Prior to installation of this modification it 22.11.2<strong>01</strong>0<br />
<strong>EASA</strong>.E.S.<strong>01</strong>0<strong>01</strong><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 />
10039707 HELICOPTERS ITALIA S.R.L.<br />
UNIPERSON<br />
AS 365N2 Installation of Audio Voice Warning on Radar<br />
Altimeter Thales AHV-8(ref. Change HI-365-34-<br />
<strong>01</strong>).<br />
10.05.2<strong>01</strong>2<br />
11.02.2005<br />
26.07.2005<br />
24.08.2005<br />
11.10.2005<br />
Limited to S/N 6414 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 />
18.05.2<strong>01</strong>2<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 269/<strong>462</strong>
Change language