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>5297 AEROSPACE DESIGN AND<br />
<strong>EASA</strong>.A.S.03847 REV. 1 A320-232 Installation of an Enhanced Surveillance Mode None Prior to installation of this modification it 09.08.2<strong>01</strong>0<br />
ENGINEERING<br />
S ATC SystemRevision of the <strong>EASA</strong> STC P-<br />
must be determined thatthe<br />
<strong>EASA</strong>.A.S.03847 to remove EWIS Limitation.<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 />
10027558 AEROSPACE DESIGN AND<br />
ENGINEERING<br />
10027628 AEROSPACE DESIGN AND<br />
ENGINEERING<br />
10029548 AEROSPACE DESIGN AND<br />
ENGINEERING<br />
10030206 AEROSPACE DESIGN AND<br />
ENGINEERING<br />
10032318 AEROSPACE DESIGN AND<br />
ENGINEERING<br />
10033237 AEROSPACE DESIGN AND<br />
ENGINEERING<br />
10039894 AEROSPACE DESIGN AND<br />
ENGINEERING<br />
10<strong>04</strong>2785 AEROSPACE DESIGN AND<br />
ENGINEERING<br />
P-<strong>EASA</strong>.A.S.03680 DHC-8-102 Traffic Alert and Collision Avoidance System<br />
(TCAS II) Installation.<br />
P-<strong>EASA</strong>.A.S.03677 REV. 1 A330-223 Introduction of a change from a 48C/182Y dual<br />
class seatingconfiguration to a 24C/242Y<br />
passenger seating configuration.<br />
REV. 1 B737-600, -700, -800, -900 Change to STC "Introduction of a Dual Battery<br />
System, MOD-0702"The change consists in<br />
removing the EWIS limitation.<br />
P-<strong>EASA</strong>.A.S.03549 B747-400 Reconfiguration of compartment zone A in<br />
accordance with AerodecModification<br />
summary MOD-0386 Rev. B dated 29 March<br />
2<strong>01</strong>0 or laterapproved revision.This STC<br />
validates FAA STC ST<strong>01</strong>829SE.<br />
Prior to installation of this modification the 09.10.2009<br />
installer must determinethat the<br />
interrelationship between this modification<br />
and any otherpreviously installed<br />
modification will introduce no adverse<br />
effect uponthe airworthiness of the<br />
product. The installati<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 />
03.12.2009<br />
The STC holder shall monitor all documentary<br />
changes of the basic AFMand related<br />
operational documentation issued by the TCholder<br />
to assurethat those documents remain<br />
suitable to be used operationally for<br />
theinstallation of dual batteries under this STC.<br />
Prior to installation of this modification it 03.11.2<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 Jamco America Inc. Instructions for<br />
Continued Airworthiness,<br />
documentnumber JD-09AC03 Rev. New,<br />
dated March 06, 2008 or later<br />
approvedrevisions must be made<br />
available to the operator at the time<br />
ofinstallation. <strong>EASA</strong> STC<br />
<strong>EASA</strong>.IM.A.02858 must be incorporated<br />
02.06.2<strong>01</strong>0<br />
DHC-8-4<strong>01</strong>, DHC-8-402 Installation of Ground Recognition Lights 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 />
27.10.2<strong>01</strong>0<br />
B767-300 Installation of First Class Seating 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 />
05.<strong>01</strong>.2<strong>01</strong>1<br />
REV. 1 A330-243 Revise the passenger seat place cabin<br />
configuration from8FC/24JCL/183YCL (215<br />
pax) to 8FC/247YCL (255 pax) passenger<br />
placestogether with associated changes to the<br />
complete aircraft interior.Installation of 64<br />
passenger places of newly manufactured<br />
Sicma Ae<br />
747-400 Certification of drainmast p/n 24E507589G02<br />
against 25.1455 on Boeing747-467ERF MSN<br />
37299 in order to nullify Hong Kong Civil<br />
AviationDepartment Variation No<br />
VAR/2<strong>01</strong>2/133.<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 />
31.05.2<strong>01</strong>2<br />
STC is only valid for B747-467F MSN37299 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 />
18.12.2<strong>01</strong>2<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 37/<strong>462</strong>
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