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 />
10<strong>01</strong>5758 ASSOCIATED AIR CENTER <strong>EASA</strong>.IM.A.S.<strong>01</strong>793 FAA STC ST10546SC AIRBUS A319-115 VIP Cabin modification This STC is limited to the A319 CJ MSN<br />
2592.Instructions for Continued Airworthiness<br />
(ICAW), Chapter 3 "Airworthiness Limitations"<br />
ref. 2350050090, revision A dated June 8,<br />
2006 or later <strong>EASA</strong> approved revision.<br />
13.06.2006<br />
10<strong>01</strong>5490 ASSOCIATED AIR CENTER, L.P. <strong>EASA</strong>.IM.A.S.<strong>01</strong>252 FAA STC ST1<strong>04</strong>74SC AIRBUS A319-133 Installation of an Executive Style Interioracc.:<br />
MDL 2300000091 Rev. D<br />
10<strong>01</strong>5924 ASSOCIATED AIR CENTER, L.P. <strong>EASA</strong>.IM.A.S.02059 REV. 2 FAA STC ST10593SC AIRBUS A319-115 Revision to <strong>EASA</strong> STC reference<br />
<strong>EASA</strong>.IM.A.S.02059 - Introduction of revised<br />
Instructions for Continued Airworthiness.STC<br />
<strong>EASA</strong>.IM.A.S.02059 - Installation of an<br />
Executive Style Interior (reference FAA STC<br />
ST10593SC dated 6 February 2007).First<br />
10<strong>01</strong>5975 ASSOCIATED AIR CENTER, L.P. <strong>EASA</strong>.IM.A.S.02126 FAA STC ST10613SC AIRBUS A319-115<br />
installation i<br />
Executive style interior (validation of FAA STC<br />
ST10613SC)<br />
10<strong>01</strong>6150 ASSOCIATED AIR CENTER, L.P. <strong>EASA</strong>.IM.A.S.02352 FAA STC ST10536SC AIRBUS A319-115 Installation of an Executive Style Interior in<br />
accordance with Master Document List,<br />
Document Number 2459000000, Revision IR,<br />
dated25 October 2007, or later <strong>EASA</strong><br />
approved revision.First installation is on MSN<br />
2837<br />
10027816 ASSOCIATED AIR CENTER, L.P. P-<br />
<strong>EASA</strong>.IM.A.S.03147<br />
REV. 1 FAA STC ST10895SC-D A319-115 Major Change to the <strong>EASA</strong> STC 10027816<br />
(FAA STC ST10895SC-D) to introducethe<br />
Decrane's side facing divan (FAA STC<br />
ST<strong>01</strong>450CH) within the"Executive Style<br />
Interior" configuration.<br />
1) Ref.: 2300021090 Rev. IR2) Limited to S/N<br />
2192Note: The airplane is limited to private use<br />
only unless the cabin door is rendered<br />
inoperable.<br />
1. The aircraft is limited to Private use only (not<br />
to be operated for hire, reward or common<br />
carriage).2. This STC is approved only for the<br />
product configuration as defined in the above<br />
Master Document List.3. Limitations and<br />
Conditions specified in FAA S<br />
Instruction for Continued Airworthiness,<br />
Chapter 3 "Airworthiness Limitation", ref.<br />
2393050090, dated March 8, 2007 or later<br />
approved revision<br />
The aircraft is limited to Private use only (not to<br />
be operated for hire, reward or common<br />
carriage).This STC is approved only for the<br />
product configuration as defined in the above<br />
Master Document List.Limitations and<br />
Conditions specified in FAA STC ST1053<br />
This approval is limited only to the installation<br />
made in Airbus ModelNumber A319-115,<br />
Serial Number 3133<br />
10030326 ASSOCIATED AIR CENTER, L.P. FAA STC ST10900SC-D A319-115 Installation of an Executive Interior This approval is limited to only the installation<br />
made in Airbus ModelNumber A319-115,<br />
Serial Number 3957Airworthiness Limitation<br />
10035731 ASSOCIATED AIR CENTER, L.P. REV. 1 FAA STC ST10906SC-D A319-115 Installation of an Executive Style Interior<strong>EASA</strong><br />
validation of FAA STC ST10906SC-D<br />
10035915 ASSOCIATED AIR CENTER, L.P. FAA STC ST10903SC-D A319-133 Modification of an Executive Interior<strong>EASA</strong><br />
Validation of FAA STC ST10903SC-D<br />
10036081 ASSOCIATED AIR CENTER, L.P. REV. 2 FAA STC ST10897SC-D B737-700 Change to <strong>EASA</strong> STC 0<strong>01</strong>0036081<br />
(Installation of an Executive Interior<br />
onB737700IGW aircraft : Project No.AAC-08-<br />
06-DAS): Installation of theERDA Model 4402<br />
Single occupant Side facing divan.<br />
inspection to be performed in all the locationsof<br />
the Cabin Interior Primary Structure Elements<br />
attachments for every3000 FC u<br />
21.11.2005<br />
14.05.2009<br />
19.03.2007<br />
30.10.2007<br />
Prior to installation of this modification it 11.07.2<strong>01</strong>2<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 />
Prior to installation of this modification it 10.06.2<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 />
restricted to MSN 3542 As per FAA STC ST10906SC-DPrior 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 no adverse<br />
effectupon the airworthin<br />
Restricted to MSN 910 As per FAA STC ST10903SC-DPrior 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 no adverse<br />
effectupon the airworthin<br />
1) This approval is limited to Aircraft B737-700,<br />
Serial number 36027.2) The aircraft operator<br />
must perform the instructions for<br />
continuedairworthiness and comply with the<br />
Airworthiness Limitation Items as perthe<br />
Instruction Continued Airworthiness, Refere<br />
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 />
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