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>4782 GKN AEROSPACE SERVICES LIMITED <strong>EASA</strong>.A.S.02980 BOEING 737-100<br />
Number 2 Cockpit Windshields Addition of This approval provides for the installation of the<br />
19.12.2007<br />
BOEING 737-200<br />
Layers of Polyrethane Interlayer to the Existing referenced windows individually or in any<br />
BOEING 737-200C<br />
Qualified Design to improve In-Service combination.<br />
BOEING 737-300<br />
BOEING 737-400<br />
BOEING 737-500<br />
BOEING 737-600<br />
BOEING 737-700<br />
BOEING 737-700C<br />
BOEING 737-800<br />
BOEING 737-900<br />
Reliability.<br />
10036545 GKN AEROSPACE SERVICES LIMITED P-<strong>EASA</strong>.A.S.03492 REV. 1 B777-200, B777-200LR<br />
Installation of a GKN Aerospace designed None Replacement of a Flight Compartment 02.11.2<strong>01</strong>1<br />
B777-300, B777-300ER<br />
Boeing 777 No 1 Windshield PartNo. 10702<br />
Window Number 1 per this STC withGKN<br />
B777F<br />
(LH) / 10703 (RH); or Part No. 10712 (LH) /<br />
ATS part no. 10712 (LH) / 10713 (RH)<br />
10713 (RH)<br />
together with the relevantwiring loom<br />
modification constitutes an Alternative<br />
Method of Compliance(AMOC) to the<br />
terminating action requirements of<br />
10<strong>01</strong>5318 GLOBAL AIRWORKS, Inc. <strong>EASA</strong>.IM.A.S.00254 REV. 1 FAA STC ST<strong>01</strong>626LA; <strong>EASA</strong>.IM.A.S BOMBARDIER CL-600-2B19<br />
BOMBARDIER CL-600-2C10<br />
BOMBARDIER CL-600-2D24<br />
10<strong>01</strong>6684 GLOBAL AIRWORKS, Inc. <strong>EASA</strong>.IM.A.S.C.<strong>01</strong>05<br />
9<br />
REV. 1 FAA STC ST<strong>01</strong>585LA A330-2<strong>01</strong>, A330-202, A330-203<br />
A330-223, A330-243, A330-3<strong>01</strong><br />
A330-321, A330-322, A330-323<br />
A330-341, A330-342, A330-343<br />
10<strong>04</strong>1546 GLOBAL AIRWORKS, Inc. FAA STC ST3<strong>04</strong>2CH ATR 42-200, ATR 42-300,<br />
ATR 42-320, ATR 42-500<br />
ATR 72-1<strong>01</strong>, ATR 72-102,<br />
ATR 72-2<strong>01</strong>, ATR 72-202,<br />
ATR 72-211, ATR 72-212,<br />
ATR 72-212A.<br />
Installation of Airworks Cockpit Door<br />
Prior to installation of this modification the<br />
Surveillance SystemRevision 1: Amended FAA installer must determine that the<br />
STC ST<strong>01</strong>626LA<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 />
Installation of AirWorks Cockpit Door Prior to the installation of this modification it<br />
Surveillance Systems (Validationof the FAA must be determinedthat the interrelationship<br />
STC ST<strong>01</strong>585LA). This STC installs a CDSS. between this modification and any<br />
The Revision 1 has been issued to correct the otherpreviously installed modification and/or<br />
references of AssociatedTechnical Documents. repair will introduce noadverse effect upon the<br />
airworthiness of the product.<br />
05.<strong>01</strong>.2009<br />
30.11.2<strong>01</strong>1<br />
Installation of a Global AirWorks Cockpit Door None<br />
Surveillance SystemThis STC installs a cockpit<br />
door surveillance system (CDSS) allowingcrew<br />
to view video images of the area outside the<br />
cockpit door.<br />
None 26.09.2<strong>01</strong>2<br />
10<strong>01</strong>57<strong>04</strong> GODERICH AIRCRAFT Inc. <strong>EASA</strong>.IM.A.S.<strong>01</strong>691 - BEECH B300 Artex ELT C406-N Installation. Modification limited to s/n FL-175.Maintenance<br />
must be in accordance with above Continued<br />
Airworthiness document<br />
10<strong>01</strong>5705 GODERICH AIRCRAFT Inc. <strong>EASA</strong>.IM.A.S.<strong>01</strong>692 BEECH B300 Universal UNS 1E Flight Management System<br />
Installation.<br />
Modification limited to s/n FL-175.Operation<br />
must bein accordance with Goderich Aircraft<br />
Inc. Flight Mnaual Supplement FMS05097-1<br />
Revision N/C approved 20 September 2005 or<br />
later approved revision. Maintenance must be<br />
in accordance with above Continued Air<br />
10<strong>01</strong>5886 GODERICH AIRCRAFT Inc. <strong>EASA</strong>.IM.A.S.020<strong>04</strong> O-LSA06-081/D (LSTC) BEECH 400A (HAWKER 400 XP) Cabin Entertainment Equipment Installation. This Installation is limited to the Serial No. RK-<br />
37 (Registration SE-DRS).This approval is for<br />
electrical/avionics aspects only. Structural<br />
aspects of this installation are not included and<br />
require separate approval.<br />
10<strong>01</strong>5887 GODERICH AIRCRAFT Inc. <strong>EASA</strong>.IM.A.S.02005 O-LSA06-117/D (LSTC) BEECH 400A (HAWKER 400 XP) Change in interior seating arrangement, 1. This Installation is limited to the Serial No.<br />
addition of sink to existing rear lavatory, RK-37 (Registration SE-DRS).2. Compatibility<br />
fabrication and installation of RH fwd<br />
of this modification with other previously<br />
cabinet,revision of existing LH fwd cabinet, approved modifications must be determined by<br />
revision to interior finishing details, and addition the installer.<br />
of new fuselage antenna.<br />
10<strong>01</strong>6452 GODERICH AIRCRAFT Inc. <strong>EASA</strong>.IM.A.S.02798 TCCA STC O-LSA08-056/D ISSUE 3 FALCON 10 <strong>EASA</strong> Validation of Transport Canada Limited<br />
STC O-LSA08-056/D Issue 3:Cabin<br />
Entertainment Equipment Upgrade for Falcon<br />
10 serial number 161 aircraft in accordance<br />
with Avionics Design Services Ltd. Master<br />
Drawing List MDL08009 Revision B, dated 31st<br />
March<br />
<strong>EASA</strong> STC limited to Falcon 10 serial number<br />
161 aircraftSee original Transport Canada<br />
Limited STC O-LSA08-056/D Issue 3See:<br />
Avionics Design Services Ltd. Master Drawing<br />
List MDL08009 Revision B, Issue 1, dated 31st<br />
March 2008.Goderich Aircraft Inc. Mainten<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 236/<strong>462</strong><br />
17.<strong>01</strong>.2006<br />
17.<strong>01</strong>.2006<br />
09.11.2006<br />
19.12.2006<br />
21.<strong>04</strong>.2008
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