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 />
10039322 BUTTERFIELD INDUSTRIES, INC. FAA STC SA02215SE 1. F90<br />
Inspection Panel Kit BI 95<strong>01</strong>-0<strong>01</strong>.Fabrication of None Prior to installation of this modification it 25.<strong>04</strong>.2<strong>01</strong>2<br />
2. 200, 200C, 200CT, 200T Inspection Panel Kit BI 95<strong>01</strong>-0<strong>01</strong>, in<br />
must be determined thatthe<br />
2. A200, A200C, A200CT, B200CT accordance withDrawing List BI 9025, Revision<br />
interrelationship between this modification<br />
2. B200T, 300<br />
A, dated February 17, 2<strong>01</strong>2, or laterFAA-<br />
and any other previouslyinstalled<br />
3. B200, B200C, B300<br />
approved revision; and installation in<br />
modification and/ or repair will introduce<br />
accordance with InstallationInstructions BI 90<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
10<strong>01</strong>5347 C & D INTERIORS <strong>EASA</strong>.IM.A.S.0<strong>04</strong>75 REV. 1 BOEING 737-600 C&D Interiors Stowage S1, Galley S1, Galley<br />
G2B, Galley G3B, Stowage S2, Forward<br />
lavatory, Passenger Seat Installation,<br />
Overhead Stowage Bin Installation, Sidewall<br />
Installation, PSU Installation, Passenger Seat<br />
Proximity Light installation.<br />
10<strong>01</strong>5324 C & D ZODIAC, Inc. <strong>EASA</strong>.IM.A.S.0028 REV. 3 FAA STC ST<strong>01</strong>415LA CL-600-2C10<br />
CL-600-2D24<br />
CL-600-2E25<br />
1. Subject to compliance with the provisions of<br />
Part21 Subpart E, this STC and associated<br />
data shall remain valid until surrendered,<br />
revoked or otherwise terminated.2. If transfer<br />
of this STC Certificate is requested under Part<br />
21A.116, the STC will be rei<br />
17.05.2006<br />
Flight Deck Access System (FDAS) Installation 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>1<br />
10<strong>01</strong>5346 C & D ZODIAC, Inc. <strong>EASA</strong>.IM.A.S.0<strong>04</strong>71 REV 1 FAA STC ST<strong>01</strong>056LA DC-9-81 (MD-81)<br />
Installation of Galleys, Closets, Stowages, 1. This STC is approved only for the product<br />
10.<strong>01</strong>.2007<br />
DC-9-82 (MD-82)<br />
Lavatories, Bins, Class Divider, (Movable), configuration as defined in the approved design<br />
DC-9-83 (MD-83)<br />
Sidewall Panels, Ceiling Panels,<br />
data referred to in the paragraph "Description".<br />
DC-9-87 (MD-87) MD 90-30 Coatrooms,and Passenger Service Unites Compatibility with other aircraft/engine<br />
(PSUs) Installation in accordance with C & D configurations shall be determined by the<br />
Interiors Index List No. A<strong>04</strong>, Revision A, dated installer.<br />
Ju<br />
10<strong>01</strong>5837 C & D ZODIAC, Inc. <strong>EASA</strong>.IM.A.S.<strong>01</strong>931 FAA STC ST<strong>01</strong>880LA BOEING 747-400 Installation of pantry -- 19.12.2006<br />
10<strong>01</strong>6190 C & D ZODIAC, Inc. <strong>EASA</strong>.IM.A.S.02421 REV. 1 FAA STC ST02144LA B777-200 Pantry installation P/N C8<strong>01</strong>0<strong>01</strong>-1<strong>01</strong>,P/N 1. Prior to installation of this modification the<br />
08.<strong>01</strong>.2009<br />
C8<strong>01</strong>0<strong>01</strong>-103 and P/N C8020<strong>01</strong>-1<strong>01</strong>.Revision installer must determine that the<br />
1: addition of P/N C8020<strong>01</strong>-1<strong>01</strong><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 i<br />
1003<strong>01</strong>54 C & D ZODIAC, Inc. FAA STC ST<strong>01</strong>989LA-D SEE <strong>EASA</strong> APPROVED MODEL Validation of FAA STC ST<strong>01</strong>989LA-D: None Prior to installation of this modification it 31.05.2<strong>01</strong>0<br />
LIST<br />
Adjustable Cargo Net Installation<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 />
10038766 C & D ZODIAC, Inc. FAA STC NO. ST02415LA B767-300 Interior Installation and Modification to include<br />
Center Bin, CabinCeilings and Outboard<br />
Stowage Bins.<br />
10<strong>04</strong>0831 C & D ZODIAC, Inc. FAA STC ST00869SE B757-200 Validation of FAA STC ST00869SE<br />
(Modification to Overhead Stowage<br />
Binslocated in the passenger cabin in order to<br />
extend the bins inboard).<br />
10032537 C&D ASSOCIATES, INC. FAA STC SA02816CH G58 Installation of C&D Associates<br />
Combustion Heater Part<br />
NumberCD50000K33.<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 />
12.03.2<strong>01</strong>2<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 />
30.07.2<strong>01</strong>2<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 />
12.11.2<strong>01</strong>0<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 150/<strong>462</strong>
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