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>6005 AVIATION FABRICATORS / CENTRAL <strong>EASA</strong>.IM.A.S.02168 FAA STC ST<strong>01</strong>139WI CESSNA 560 Installation of a 39-inch or a 45-inch two-place The STC covers only installation of parts<br />
divan or a 24-inch one-place divan per Aviation contained in the Description sectionUpholstery,<br />
13.09.2006<br />
Fabricators STC Data Package, AF-342, Rev covers, aisle width, oxygen, seat belts are not<br />
A, dated 12, June, 2003 and stamped "FAA<br />
Approved" with an approval date of October<br />
22, 2003 or later approved revisi<br />
covered<br />
10<strong>01</strong>5576 AVIATION FABRICATORS, Inc. <strong>EASA</strong>.IM.A.S.<strong>01</strong>487 REV. 1 FAA STC SA2629CE 200, 200C, 200CT, 200T, 300<br />
300LW, B200, B200C, B200CT<br />
B200GT, B200CGT<br />
B200T, B300, B300C<br />
Installation of two place side-facing divan. 1) Prior to installation of this modification the<br />
installer mustdetermine that the<br />
interrelationship between this modification and<br />
anyother previously installed modification will<br />
introduce no adverse effectupon the<br />
airworthiness of the product. 2) The inst<br />
1. This STC must be installed per 08.10.2009<br />
Aviation Fabricators drawing D-10265,no<br />
revision or later approved revision on<br />
airplanes manufactured after12<br />
December 1986, with nine or fewer<br />
passenger seats, including thedivan. 2.<br />
For other divan installation, Aviatio<br />
10029817 AVIATION FABRICATORS, Inc. FAA STC ST<strong>01</strong>572WI 400 Beechjet 400 Cabin Configuration. 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 />
22.<strong>04</strong>.2<strong>01</strong>0<br />
10029869 AVIATION FABRICATORS, Inc. FAA STC NO. SA00961WI PA-31-325, PA-31-350<br />
PA-31P, PA-31T, PA-31T1<br />
PA-31T2, PA-31T3, PA-31<br />
PA-42, PA-42-720, PA-42-1000<br />
Stretcher Installation per Aviation Fabricators,<br />
Inc. STC Drawing List,Doc. No. AF-2<strong>04</strong><br />
10031917 AVIATION FABRICATORS, Inc. FAA STC SA2818SW 441 Installation of 1, 2 or 3 place side seating<br />
divans in accordance withFAA STC<br />
SA2818SW<br />
10032446 AVIATION FABRICATORS, Inc. FAA STC SA2774CE 1. 200, 200C, 200CT, 200T<br />
1. A200, A200C, A200CT, B200<br />
1. B200CT, B200T, 300, 300LW<br />
2. B200C, B200CGT, B200GT<br />
2. B300, B300C<br />
10032903 AVIATION FABRICATORS, Inc. FAA STC REF SA4157SW SEE <strong>EASA</strong> APPROVED MODEL<br />
LIST<br />
Installation of Passenger Seats with Hinged<br />
Backrest.<br />
Installation of one, two, or three place side<br />
facing seat (frame only).<br />
The installer is responsible for ensuring that the<br />
installation complieswith any supplemental<br />
oxygen requirements as required for operation<br />
The installation of this modification by<br />
third persons is subject towritten<br />
permission of the approval holder and<br />
disposal of the approvedappropriate<br />
documentation.Prior to installation of this<br />
modification it must be determined<br />
27.<strong>04</strong>.2<strong>01</strong>0<br />
none<br />
thatthe interrelationship b<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 />
22.09.2<strong>01</strong>0<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 />
08.11.2<strong>01</strong>0<br />
None This STC only approves the installation of 07.12.2<strong>01</strong>0<br />
the parts contained in theabove section<br />
"associated technical documentation".<br />
The requirements forthe aisle width,<br />
passenger oxygen system, seats and<br />
safety belts, andupholstery coverings will<br />
require a separate a<br />
10<strong>01</strong>5323 AVIATION PARTNERS BOEING <strong>EASA</strong>.IM.A.S.00279 REV. 3 FAA STC ST00830SE BOEING 737-700<br />
Installation of Aviation Partners Boeing 1. Subject to compliance with the provisions<br />
30.06.2008<br />
BOEING 737-800<br />
Winglets in accordance with the following of Part 21 Subpart E, this STC and associated<br />
BOEING 737-900<br />
documents:- APB Document List AP37.7- data shall remain valid until surrendered,<br />
E620 Rev. A (737-700)- APB Document List withdrawn or otherwise terminated.2. If<br />
AP37.1- E620 Rev. A (737-700IGW)- APB transfer of this Certificate is requested under<br />
10<strong>01</strong>5659 AVIATION PARTNERS BOEING <strong>EASA</strong>.IM.A.S.<strong>01</strong>636 REV. 5 FAA STC ST<strong>01</strong>518SE B757-200, -300<br />
Document List AP37.8- E620 Rev. A (737-800)- Part 21A.116 the STC will be<br />
APB Documen<br />
Install of Aviation Partners Boeing Winglets on The Partial Wing Retrofit Installation (300-1 Kit) Prior to installation of this modification it 11.<strong>04</strong>.2<strong>01</strong>1<br />
B757-200 and B757-300Aeroplanes<br />
is approved for RollsRoyce RB211-535 must be determined thatthe<br />
powered a/c.<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>3 <strong>Page</strong> 90/<strong>462</strong>
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