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>04</strong>1380 INFLIGHT WARNING SYSTEMS, Inc. FAA STC ST02300LA B777-200, 200LR, 300, 300ER Validation of FAA STC ST02300LA related to None. Prior to installation of this modification it 12.09.2<strong>01</strong>2<br />
Installation of Fan VibrationMonitor Unit.<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 />
10<strong>04</strong>1522 INFLIGHT WARNING SYSTEMS, Inc. A318-111/-112/-121/-122<br />
A319-111/-112/-113/-114/-115<br />
A319-131/-132/-133<br />
A320-111/-211/-212/-214<br />
A320-231/-232/-233<br />
A321-111/-112/-131/-211/-212<br />
A321-213/-231/-232<br />
10<strong>01</strong>7143 ING. MIROSLAV RUSINAK S.R.O. <strong>EASA</strong>.R.S.<strong>01</strong>246 BELL 427 Installation of the articulated patient loading<br />
system into Bell 427 rotorcraft.<br />
Installation of Inflight Warning System Fan None Prior to installation of this modification it 25.09.2<strong>01</strong>2<br />
Vibration Monitor Unit (VMU)model n. 2160<strong>01</strong>-<br />
must be determined thatthe<br />
400<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 />
427-706-020-1<strong>01</strong> – Bell Helicopter Textron<br />
Cabin Hardpoints Provision Kit must be<br />
installed (BHT-427-II-27 rev 0 dated 16<br />
September 20<strong>04</strong>) prior to installation of this<br />
STC.STC <strong>EASA</strong>.IM.R.S.00548 or<br />
<strong>EASA</strong>.IM.R.S.00577 (FAA STC SR02381AT)<br />
– Installation of Pass<br />
10038518 ING. MIROSLAV RUSINAK S.R.O. P-<strong>EASA</strong>.R.S.<strong>01</strong>416 BELL 427 Support unit for medical devices 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 />
22.02.2<strong>01</strong>2<br />
10027603 INGENIEURBUERO FUER LUFTFAHRT P-<strong>EASA</strong>.R.S.<strong>01</strong>447 AS350 B1, B2, B3<br />
AS355 E, F, F1, F2, N, NP<br />
Installation of airborne laser scanning<br />
equipment in AS350/355 serieshelicopter<br />
10<strong>01</strong>5589 INNOTECH AVIATION <strong>EASA</strong>.IM.A.S.<strong>01</strong>500 TCCA/LSTC Q-LSA05-029/D BOMBARDIER BD-700-1A10 Miscellaneous modifications to cabin interior 1. Limited to S/N 9<strong>01</strong>72. Regarding the<br />
and installation of Electronic Flight Bag System installation of the Electronic Flight Bag System<br />
provisions for BD700-1A10 Global Express the design covers only the mounting device<br />
Acc.: MDL-05103002 Rev. B or later TCCA and its connection to the aircraft. The<br />
approved rev.Validation of imported<br />
suitability, integrity or accuracy of the EFB<br />
TCCA/LSTC: Q-LSA05-029/D<br />
hardware, software, database, dis<br />
10<strong>01</strong>59<strong>04</strong> INNOTECH AVIATION <strong>EASA</strong>.IM.A.S.02030 TCCA LSTC Q-LSA06-026/D ISS 1 BD-700-1A10 Modification of EGPWS Radar Altimeter<br />
Callouts and installationof the IPOD on ACSN<br />
9163Valdiation of TCCA Limited STC Q-<br />
LSA06-26/D to S/N 9163MDL: 26126002 Rev<br />
NC or later approved revisionsTCCA SoC:<br />
NAI5<strong>01</strong>2-06-0063 dated June 20, 2006<br />
10<strong>01</strong>6130 INNOTECH AVIATION <strong>EASA</strong>.IM.A.S.02324 TCCA STC Q-LSA06-<strong>01</strong>8D BOMBARDIER BD-700-1A10 Re-Locate Electronic Flight Bag and<br />
Miscellaneous Cabin Modifications in Cockpit<br />
of SN 9145Validation of TCCA Limited STC<br />
Q-LSA06-<strong>01</strong>8/D to S/N 9145MDL: 26115002<br />
Rev A or later TCCA approved<br />
revisionsCompliance Plan: CP26115-0<strong>01</strong><br />
10<strong>01</strong>6228 INNOTECH AVIATION <strong>EASA</strong>.IM.A.S.02480 TCCA STC Q-LSA07-029/D BD-700-1A11 Installation of Photosmart printer and<br />
installation of additional handset for in the aft<br />
lhs of SN 92<strong>04</strong>Validation of TCCA Limited STC<br />
Q-LSA07-029/D to S/N 92<strong>04</strong><br />
10<strong>01</strong>6277 INNOTECH AVIATION <strong>EASA</strong>.IM.A.S.02566 Q-LSA07-035/D BD-700-1A11 Miscellaneous Cabin Modifications on SN<br />
9188Validation of TCCA Limited STC Q-<br />
LSA07-035/D to S/N 9188MDL:<br />
MDL27124002Compliance Plan: CP27124-0<strong>01</strong><br />
Rev. A<br />
10<strong>01</strong>6407 INNOTECH AVIATION <strong>EASA</strong>.IM.A.S.02737 TCCA STC Q-LSA08-0<strong>01</strong>/D BOMBARDIER BD-700-1A10 Replacement of conference table in aircraft<br />
S/N 9197, aft cabin.<br />
19.02.2007<br />
Service Bulletin No. 25.00.62 is a prerequisite Prior to installation of this modification it 13.10.2009<br />
and must be installedprior this modification Any must be determined thatthe<br />
alteration of installed equipment leads to interrelationship between this modification<br />
noncompliance ofcommitted and approved and any other previouslyinstalled<br />
design and therefore requires reinvestigation modification and/ or repair will introduce<br />
undchange approval prior use.<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
Restricted to ASN 9197With this modification<br />
incorporated Aft LSH forward facing double<br />
seats must not be occuped durint taxi take off<br />
and landing.<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 278/<strong>462</strong><br />
18.11.2005<br />
28.07.2006<br />
22.03.2007<br />
21.<strong>01</strong>.2008<br />
12.10.2007<br />
19.03.2008
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