04/01/2013 Page 1/462 - EASA
04/01/2013 Page 1/462 - EASA
04/01/2013 Page 1/462 - EASA
Create successful ePaper yourself
Turn your PDF publications into a flip-book with our unique Google optimized e-Paper software.
<strong>EASA</strong> STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue<br />
10039313 AMTECH AERONAUTICAL LIMITED REV. 1 TCCA STC C-LSA06-188/D MF900 Artex C406-N ELT and Flight Displays FD600 Limited to S/N 141 Prior to installation of this modification it 27.<strong>04</strong>.2<strong>01</strong>2<br />
Video Camera Installations.<strong>EASA</strong> validation of<br />
must be determined thatthe<br />
TCCA Limited STC No C-LSA06-188/D Issue<br />
interrelationship between this modification<br />
1 dated 23May 2006.<br />
and any other previouslyinstalled<br />
modification and/ or repair will introduce<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
10<strong>01</strong>5619 ANCRA INTERNATIONAL LLC <strong>EASA</strong>.IM.A.S.<strong>01</strong>571 ST<strong>01</strong>748LA BOEING 757-200 Installation of a Main Deck Cargo Handling<br />
System<br />
10<strong>01</strong>5736 ANCRA INTERNATIONAL LLC <strong>EASA</strong>.IM.A.S.<strong>01</strong>760 ST116<strong>04</strong>LA-T BOEING 747-400 SERIES Installation of Main Deck Cargo Loading<br />
System<br />
<strong>EASA</strong> STC <strong>EASA</strong>.IM.A.S.02<strong>04</strong>0 must be<br />
installed in conjunction with this installation.<br />
10<strong>01</strong>5739 ANCRA INTERNATIONAL LLC <strong>EASA</strong>.IM.A.S.<strong>01</strong>763 ST<strong>01</strong>644LA AIRBUS A300-600 <strong>EASA</strong> validation of FAA STC<br />
This STC is only applicable on Airbus A300-<br />
ST<strong>01</strong>644LA:revision C to Ancra Controlled 600 aircraft converted to freighter in<br />
Drawing List DL83690STC ST<strong>01</strong>644LA, cargo accordanace with <strong>EASA</strong>.A.S.00387/FAA STC<br />
Loading Sytem,Project Number SA11805LA-T ST<strong>01</strong>431NYThe aircraft must be compliant<br />
with the instructions for continued airworthiness<br />
(see ANCRA reports 8967 revision A and 8284<br />
10<strong>01</strong>5953 ANCRA INTERNATIONAL LLC <strong>EASA</strong>.IM.A.S.02095 REV. 1 FAA STC ST<strong>01</strong>926LA BOEING 747-400 Installation of Main Deck Cargo Loading<br />
System<br />
10<strong>01</strong>6063 ANCRA INTERNATIONAL LLC <strong>EASA</strong>.IM.A.S.02242 FAA STC ST<strong>01</strong>551LA AEROSPATIALE ATR 42-300 Installation of Ancra mechanical main deck<br />
AEROSPATIALE ATR 42-320 cargo landing system<br />
10<strong>01</strong>6114 ANCRA INTERNATIONAL LLC <strong>EASA</strong>.IM.A.S.023<strong>04</strong> FAA STC ST<strong>01</strong>890LA BOEING B737-400 Installation of cargo loading system in<br />
accordance with FAA approved Ancra<br />
International LLC Controlled Drawing List<br />
DL84670-10, Revision B, dated March 22,<br />
2006, or later FAA approved revision.<br />
10<strong>01</strong>6408 ANCRA INTERNATIONAL LLC <strong>EASA</strong>.IM.A.S.02739 FAA STC ST<strong>01</strong>388LA BOEING 747-200<br />
BOEING 747-300<br />
BOEING 747-400<br />
BOEING 767-200 SERIES<br />
BOEING 767-300 SERIES<br />
BOEING 767-400<br />
BOEING 767-400ER<br />
BOEING 777-200<br />
BOEING 777-300<br />
Installation of Power Drive Unit (Cargo<br />
System).<br />
10<strong>01</strong>6473 ANCRA INTERNATIONAL LLC <strong>EASA</strong>.IM.A.S.02819 FAA STC ST00680DE BOEING B737-400 Installation of mechanical cargo loading system<br />
Part Number84980-10 & -20 on B737-400<br />
aircraft<br />
<strong>EASA</strong> STC <strong>EASA</strong>.IM.A.S.02039 must be<br />
installed in conjunction with this installation.This<br />
STC is approved only for the product<br />
configuration as defined in the approved design<br />
data referred to in the paragraphs "Description"<br />
and “Associated Technical Document<br />
1. STC SA 2968SO (<strong>EASA</strong>.IM.A.S.02423),<br />
SA2969SO (<strong>EASA</strong>.IM.A.S.02424), and<br />
SA2970SO (<strong>EASA</strong>.IM.A.S.02425) must be<br />
installed in conjunction with this installation.2.<br />
This STC is approved only for the product<br />
configuration as defined in the approved design<br />
1. 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 />
10028464 ANCRA INTERNATIONAL LLC FAA STC ST02279LA B767-300 Install Main Deck Cargo Loading System<br />
airworthiness of the product.2.<br />
To be installed on a/c converted by IAI<br />
Freighter Conversion (<strong>EASA</strong> STC10028430)<br />
23.12.2005<br />
27.06.2006<br />
07.<strong>04</strong>.2006<br />
12.<strong>01</strong>.2007<br />
08.12.2006<br />
18.<strong>04</strong>.2007<br />
31.03.2008<br />
02.03.2009<br />
Prior to installation of this modification it 13.<strong>01</strong>.2<strong>01</strong>0<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 />
10030694 ANCRA INTERNATIONAL LLC FAA STC ST023<strong>04</strong>LA B737-300 Installation of main deck cargo loading system. None This modification does not effect<br />
Electrical Wiring InterconnectionSystems<br />
This modification does not effect or<br />
create Fatigue Critical StructuresThe<br />
STC <strong>EASA</strong>.IM.A.S.<strong>01</strong>754 (FAA<br />
ST<strong>01</strong>827LA) must be installed<br />
inconjunction with this installation.Prior to<br />
inst<br />
<strong>01</strong>.07.2<strong>01</strong>0<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 76/<strong>462</strong>
Change language