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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>5911 ISRAEL AEROSPACE INDUSTRIES, <strong>EASA</strong>.IM.A.S.02<strong>04</strong>0 REV. 1 BOEING 747-400 Conversion of Boeing 747-400 Aircraft from 1. Supplementary Data Sheet<br />

27.06.2007<br />

LTD. I<br />

Combi to Special Freighter Configuration TCDS.IM.A.A.02<strong>04</strong>0 applies,2. This STC is<br />

approved only for the product configuration as<br />

defined in the approved design data referred to<br />

in the paragraph "Description". Compatibility<br />

with other aircraft/engine configuration<br />

10028430 ISRAEL AEROSPACE INDUSTRIES,<br />

LTD. I<br />

P-<br />

<strong>EASA</strong>.IM.A.S.02477<br />

REV. 3 CAAI STC SA218 B767-300 Conversion of Boeing B767-300 from<br />

Passenger Configuration to SpecialFreighter<br />

(BDSF) with Main Deck Class E Cargo<br />

Compartment.<br />

An approved Cargo Loading System must be<br />

installed.<br />

10<strong>01</strong>5652 ITOCHU AIRLEASE, INC. <strong>EASA</strong>.IM.A.S.<strong>01</strong>627 ST1<strong>04</strong>36SC BOEING 767-300 Reconfiguration of an existing three seating<br />

class interior with 199 passengers to a two<br />

seating class interior (enconomy & business<br />

seats) with 232 passengers.<br />

10<strong>01</strong>4840 J & C ENGINEERING SERVICES LTD <strong>EASA</strong>.A.S.03057 BOEING B737-300 TCAS II Installation Limited to installation on Boeing 737-300 MSN<br />

28740.Compatibility of this design change with<br />

other previously approved modifications must<br />

be determined by the installer.<br />

10<strong>01</strong>4841 J & C ENGINEERING SERVICES LTD <strong>EASA</strong>.A.S.03058 BOEING B737-300 Installation of Driessen Galley No 1 Limited to installation on Boeing 737-300 MSN<br />

28740.Compatibility of this design change with<br />

other previously approved modifications must<br />

be determined by the installer.<br />

10<strong>01</strong>5174 J & C ENGINEERING SERVICES LTD <strong>EASA</strong>.A.S.03547 REV 1 R2160, R2160D, R2160I, R2120U Removal of VFR Limitation from AFM<br />

Approved Operation Section.<br />

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 />

airworthiness of the product. The install<br />

Incorporation of this STC constitutes an 20.11.2<strong>01</strong>2<br />

AMOC for the list of affectedADs as<br />

published in the TCDS Supplement. Prior<br />

to installation of this modification it must<br />

be determined thatthe interrelationship<br />

between this modification and any other<br />

previouslyinst<br />

10<strong>01</strong>5175 J & C ENGINEERING SERVICES LTD <strong>EASA</strong>.A.S.03550 BOEING 767-200 Approval of Galley and Crew Rest Installation. 12.06.2008<br />

10<strong>01</strong>5356 JAMCO AMERICA INC <strong>EASA</strong>.IM.A.S.00647 FAA STC ST<strong>01</strong>372SE BOEING 767-300 New Seats and Interior Reconfiguration 1. Limitation on FAA STC in respect of<br />

concurrent installation of Thales IFE STC<br />

ST<strong>01</strong>62LA is not applicable2. This STC is<br />

approved only for the product configuration as<br />

defined in the approved design data referred to<br />

in the paragraph "Description". Compati<br />

10<strong>01</strong>5496 JAMCO AMERICA INC <strong>EASA</strong>.IM.A.S.<strong>01</strong>258 FAA STC ST<strong>01</strong>121SE BOEING 767-200<br />

BOEING 767-300<br />

BOEING 767-400ER<br />

10<strong>01</strong>6<strong>04</strong>0 JAMCO AMERICA INC <strong>EASA</strong>.IM.A.S.02209 REV. 1 FAA STC ST<strong>01</strong>700SE BOEING 747-400 Removal of the strengthened flight deck door<br />

and modification and reinstallation of luggage<br />

bins on the upper deck in accordance with<br />

Jamco Aero Design & Engineering Master<br />

Drawing List JD-03AC02 Rev. F or later<br />

revisions of the above listed documents appr<br />

Installation of a new security flight deck door 1. This STC is approved only for the product<br />

configuration as defined in the approved design<br />

data referred to in the paragraph "Description".<br />

Compatibility with other aircraft/engine<br />

configurations shall be determined by the<br />

installer.<br />

1. This STC is limited to the following aircraft<br />

after incorporation of Boeing SB 747-00-20<strong>04</strong><br />

Passenger to Freighter conversion:a. RT5<strong>01</strong><br />

Sn. 24061b. RT506 Sn. 24066c. RT507<br />

Sn. 24226d. RT509 Sn. 249752. This<br />

STC is<br />

10<strong>01</strong>6307 JAMCO AMERICA INC <strong>EASA</strong>.IM.A.S.026<strong>04</strong> FAA STC ST<strong>01</strong>459SE BOEING 767-300 Oxygen Module Installation. Reconfiguration of Passenger seats as per<br />

FAA STC SA7032NM-D must be installed<br />

concurrently. This FAA STC must be<br />

approved by <strong>EASA</strong>directly or by Grandfather<br />

Rights before installation on a <strong>EASA</strong> member<br />

state aircraft.<br />

10<strong>01</strong>6541 JAMCO AMERICA INC <strong>EASA</strong>.IM.A.S.02919 FAA STC ST00240SE ; P. GILLESP BOEING 747-200 Installation of Jamco Galley in accordance with Prior to installation of this modification the<br />

Jamco America Inc. Master Drawing List IA- installer must determine that the<br />

036, Rev. A dated September 1, 1995, or later interrelationship between this modification and<br />

approved revisions.<br />

any other previously installed modification will<br />

introduce no adverse effect upon the<br />

airworthiness of the product.The interior<br />

<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 283/<strong>462</strong><br />

02.11.2005<br />

29.05.2007<br />

31.05.2007<br />

07.11.2008<br />

17.03.2005<br />

21.06.2005<br />

02.<strong>04</strong>.2007<br />

10.<strong>01</strong>.2008<br />

16.<strong>01</strong>.2009

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