04/01/2013 Page 1/462 - EASA

EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue
10014919 AIM AVIATION (JECCO) LIMITED EASA.A.S.03165 JAA/25/03/028 ISSUE 1 BOEING 747-400 Virgin Atlantic Airways B747-400 CoCo The following EASA approved STC's must be
09.10.2007
Reconfiguration.
installed concurrently with this design
change:EASA.A.S.02860EASA.IM.A.S.02572
10015102 AIM AVIATION (JECCO) LIMITED EASA.A.S.03445 Premium Cabins UpgradeAppearance, comfort Prior to installation of this modification the
and maintenance improvement changes to the installer must determine that the
seats and the window reveals and shades in interrelationship between this modification and
the First and Business Class cabins.
any other previously installed modification will
introduce no adverse effect upon the
airworthiness of the product. The install
10015103 AIM AVIATION (JECCO) LIMITED EASA.A.S.03446 REV. 1 AIRBUS A330-243 Major Change to STC EASA.A.S.03446 (AIM
Major Change MM384-07)date of issue 14
November 2008.Introduce decorative finish
change to Contour 0995 series BusinessClass
Seats.
10040431 AIM AVIATION (JECCO) LIMITED 747-400 Installation of a single isolation switch in
accordance with AIMAviation Service Bulletin
B747-24-011 dated April 23, 2012
asreplacement for AIM Aviation Service
Bulletin B747-24-04 or B747-24-05in order to
comply to FAA AD 2009-15-12.
EASA Supplemental Type Certificate
EASA.A.S.03446 (AIM Major ChangeMM384-
07) must be embodied prior to the installation
of this MajorChange.As per indications stated
in AIM MAJOR Change ref. Doc. MM481-10
IssueC.
05.08.2008
Prior to installation of this modification it 22.12.2010
must be determined thatthe
interrelationship between this modification
and any other previouslyinstalled
modification and/ or repair will introduce
no adverse effectupon the airworthiness
of the product.
none Flight Manual Supplement AIM Aviation
Document Nr 11184 Issue A, dated28
May, 2012 shall be on board the modified
aircraft.Prior to installation of this
modification it must be determined
thatthe interrelationship between this
modification and any other pr
03.07.2012
10015599 AIM AVIATION INC. EASA.IM.A.S.01535 ST01504SE BOEING 757-200 Installation of a Flight Deck Galley 03.04.2006
10015600 AIM AVIATION INC. EASA.IM.A.S.01536 FAA STC ST01490SE BOEING 757-200 SERIES Installation of a Flight Deck Lavatory This STC is approved only for the product
configuration as defined in the approved design
data referred to in the paragraph "Description".
Compatibility with other aircraft/engine
configurations shall be determined by the
installer.
31.03.2006
10014775 AIR ALLIANCE GmbH EASA.A.S.02973 SOCATA TBM 700 Installation of Garmin GTX330D Transponder Prior to installation of this modification the
15.08.2007
with Top Antenna.
installer must determine that the
interrelationship between this modification and
any other previously installed modification will
introduce no adverse effect upon the
airworthiness of the product. The install
10014857 AIR ALLIANCE GmbH EASA.A.S.03081 REV. 3 CESSNA 208
CESSNA 208A
CESSNA 208B
Conversion of airplane for parachute
operations.Installation of PARAKIT NAY001 or
ParaKit C208-83 00 00 "System Gomolzig".
Prior to installation of this modification the
installer must determine that the
interrelationship between this modification and
any other previously installed modification will
introduce no adverse effect upon the
airworthiness of the product. The install
10014947 AIR ALLIANCE GmbH EASA.A.S.03207 PIPER PA-42 Installation of TCAS 9900 BX. 06.12.2007
10014988 AIR ALLIANCE GmbH EASA.A.S.03281 PIPER PA-31T1 Installation of Avionic Upgrade according MDL
2007_019_2029 AA Form 1 Rev. 0.
10.01.2008
10015178 AIR ALLIANCE GmbH EASA.A.S.03556 REV. 1 BEECH 300 Installation of L3 FDR1000; Collins EGPWS Prior to installation of this modification the
20.06.2008
Mark VI; Honeywell CAS 67 & Dual MST 67A installer must determine that the
Mode S Diversity Transponder; Artex 406-2 interrelationship between this modification and
ELT
any other previously installed modification will
introduce no adverse effect upon the
airworthiness of the product.The installa
10015205 AIR ALLIANCE GmbH EASA.A.S.03606 CESSNA 525
CESSNA 525A
Exchange of GPS Navigation System KING
KLN 900 against Flight Management System
Universal UNS 1Lw
10015226 AIR ALLIANCE GmbH EASA.A.S.03643 REV. 1 CESSNA 525 Installation of Dual GTX 330D as Replacement
of Dual KT 70 or KT 71
1. This STC is only eligible for aeroplanes
equipped with GPS Receiver System KLN
900 and Collins Pro Line 21 Avionic
System2.Prior to installation of this modification
the installer must determine that the
interrelationship between this modific
Prior to installation of this modification the
installer must determine that the
interrelationship between this modification and
any other previously installed modification
will introduce no adverse effect upon the
airworthiness of the product.
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