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 />
10030755 AEROSERVIS, S.R.O. P-<strong>EASA</strong>.A.S.03873 SF340A Installation of Universal UNS-1Msp Flight Valid for Saab SF340A/s/n 340.026 and 1.,,Prior to installation of this modification 03.07.2009<br />
management System<br />
340.038 only.<br />
the installer mustdetermine that the<br />
interrelationship between this modification<br />
and anyother previously installed<br />
modification will introduce no adverse<br />
effectupon the airworthiness of the<br />
product.2.,,The ins<br />
10<strong>01</strong>5200 AEROSPACE DESIGN AND<br />
CERTIFICATION<br />
10<strong>01</strong>5246 AEROSPACE DESIGN AND<br />
CERTIFICATION<br />
10030093 AEROSPACE DESIGN AND<br />
CERTIFICATION<br />
10031738 AEROSPACE DESIGN AND<br />
CERTIFICATION<br />
10032496 AEROSPACE DESIGN AND<br />
CERTIFICATION<br />
10032541 AEROSPACE DESIGN AND<br />
CERTIFICATION<br />
10034447 AEROSPACE DESIGN AND<br />
CERTIFICATION<br />
10037643 AEROSPACE DESIGN AND<br />
CERTIFICATION<br />
10038646 AEROSPACE DESIGN AND<br />
CERTIFICATION<br />
10039615 AEROSPACE DESIGN AND<br />
CERTIFICATION<br />
10<strong>04</strong><strong>01</strong>89 AEROSPACE DESIGN AND<br />
CERTIFICATION<br />
<strong>EASA</strong>.A.S.03592 AIRBUS A320-232 A320 In Flight Entertainment – IFE – Upgrade Prior to installation of this modification the<br />
installer must determine that the<br />
interrelationship between this modification and<br />
any other previously installed modification<br />
will introduce no adverse effect upon the<br />
airworthiness of the product.<br />
29.10.2008<br />
<strong>EASA</strong>.A.S.03683 DIAMOND DA-42 Banbury Modification 0<strong>01</strong> - FLIR Installation. 1. Prior to installation of this modification the<br />
installer must determine that the<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 />
07.11.2008<br />
BAE 146-200 New Cabin Configuration None None 21.05.2<strong>01</strong>0<br />
P-<strong>EASA</strong>.R.S.<strong>01</strong>593 AS 350 B, D, B1, B2, BA, BB<br />
AS 350 B3<br />
B300 Review of modifications installed prior to import Aircraft Serial Number FL-327 Only 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 />
09.09.2<strong>01</strong>0<br />
Installation of Indraero Siren IS10-100 Cargo<br />
Hook<br />
P-<strong>EASA</strong>.A.S.03947 BOEING 767-341 Review of modifications installed prior to import Limitations as per associated technical<br />
(B767-341 Installationof SELL Galley, Crew documentation:- Flight Manual Supplement,<br />
Rest, 221 LOPA & ELT)<br />
doc. JN189 ADC29 Issue 1 dated 16/11/09-<br />
Instructions for Continued Airworthiness, doc.<br />
JN189 ADC54-25 Issue 5dated<br />
14/10/2<strong>01</strong>0.Restricted to S/N 24753<br />
REV. 1 B737-700 Cabin certification for aircraft use in<br />
Commercial operations<br />
A330-243 Installation of new Business Class Avio EBIZ<br />
Seats and IMS Rave IFESystem. The FWD<br />
cabin is currently configured with BC and EY<br />
seats which are tobe removed and replaced<br />
with new Avio BC seats. The MAS 200E IFE<br />
systemwill be removed from the FWD Cabin<br />
and<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 />
11.11.2<strong>01</strong>0<br />
Refer to AFM supplement JN314-002 ADC29<br />
Issue 1<br />
MBB-BK 117 B-2 Installation of LTS1<strong>01</strong>-850B-2 Engines into<br />
MBB-BK117 B-2 Helicopter<br />
B200 KING AIR Installation of polyurethane reticulated foam This STC grants no credit for any fuel tank<br />
into fuel tanks, asdefined by:JN323 ADC17 (1) flammability reduction.<br />
Master Data List<br />
Prior to installation of this modification it 15.11.2<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 />
Prior to installation of this modification it 12.<strong>04</strong>.2<strong>01</strong>1<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 />
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 />
13.12.2<strong>01</strong>1<br />
None None 05.03.2<strong>01</strong>2<br />
Prior to installation of this modification it 14.05.2<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 />
B757-200 Installation of VIP Bedroom and Bathroom None None 15.06.2<strong>01</strong>2<br />
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