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 />
1003<strong>462</strong>3 AIRPLUS MAINTENANCE GmbH 112, 112B, 112TC, 112TCA Dual installation of Garmin<br />
None The antenna installation is not covered by 15.<strong>04</strong>.2<strong>01</strong>1<br />
114, 114A, 114B, 114TC GNS430(A)W/GNS530(A)W(TAWS)<br />
this STC. The aircraft musthave been<br />
already equipped with suitable antennas.<br />
Prior to installation of this modification it<br />
must be determined thatthe<br />
interrelationship between this modification<br />
and any other prev<br />
10035120 AIRPLUS MAINTENANCE GmbH P-<strong>EASA</strong>.A.S.03596 DHC-8-315 VIP Cabin Interior Modification as detailed in Installation is limited to DHC-8-315, S/N 0348 V-Plane engineering GmbH, DOA <strong>EASA</strong> 26.05.2<strong>01</strong>1<br />
AIRplus DescriptionDocument DE-0348-<br />
21J.323 shall fulfil the obligationsof Part<br />
2500<strong>01</strong>, Revision 3, dated 03.05.2<strong>01</strong>1<br />
21, Paragraph 21A.3. Prior to installation<br />
of this modification it must be determined<br />
thatthe interrelationship between this<br />
modification and any other<br />
previouslyinstalled modif<br />
10036129 AIRPLUS MAINTENANCE GmbH SEE <strong>EASA</strong> APPROVEL MODEL<br />
LIST<br />
10037559 AIRPLUS MAINTENANCE GmbH SEE <strong>EASA</strong> APPROVED MODEL<br />
LIST<br />
Installation of Honeywell EGPWS MK VI<br />
System<br />
10038318 AIRPLUS MAINTENANCE GmbH 500 Installation of Garmin Transponder GTX 330D<br />
on Cessna 500 Series./ Installation of Garmin<br />
Mode A/C/S Transponder GTX 330D with<br />
additionaldiversity antenna.<br />
The aircraft must have been already equipped<br />
with a suitable display andsuitable sensors.<br />
Prior to installation of this modification it 12.08.2<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 />
Installation of Garmin G600 Avionics System None The Aircraft must have been already<br />
equipped with a suitable GPSReceiver.<br />
Autopilot Coupling is not covered by this<br />
STC. Prior to installation of this<br />
modification it must be determined<br />
thatthe interrelationship between this<br />
modification and any other prev<br />
06.12.2<strong>01</strong>1<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 />
06.02.2<strong>01</strong>2<br />
10<strong>01</strong>4468 AIRTOURING LTD <strong>EASA</strong>.A.S.02529 CESSNA 441 SERIES Installation of Dual GTX330D, RDR2000,<br />
MX20, KN63 & KGP-560 TAWS<br />
-- 11.08.2006<br />
10<strong>01</strong>4591 AIRTOURING LTD <strong>EASA</strong>.A.S.02702 PIPER PA-31-350 Installation of Avionics Upgrade -- 28.07.2006<br />
10<strong>01</strong>4717 AIRTOURING LTD <strong>EASA</strong>.A.S.02893 SOCATA TB 10<br />
Installation of Honeywell KGP560 Class B This STC is approved only for the product<br />
12.12.2006<br />
SOCATA TB 20<br />
TAWS<br />
configuration as defined in the approved design<br />
SOCATA TB 200<br />
data referred to in the paragraph "Description".<br />
SOCATA TB 21<br />
Compatibility with other aircraft/engine<br />
SOCATA TB 9<br />
configurations shall be determined by the<br />
SOCATA TB.20GT<br />
installer.<br />
10<strong>01</strong>4740 AIRTOURING LTD <strong>EASA</strong>.A.S.02923 BEECH B200 Installation of KGP560 TAWS and Dual This STC is approved only for the product<br />
05.03.2007<br />
GTX330D Mode S<br />
configuration as defined in the approved design<br />
data referred to in the paragraphs "Description"<br />
and “Associated Technical Documentation”.<br />
Compatibility with other aircraft/engine<br />
configurations shall be determined<br />
10<strong>01</strong>4874 AIRTOURING LTD <strong>EASA</strong>.A.S.03099 CESSNA CITATION CS 551 Installation of Avionic Upgrade Requires prior embodiment of Gamma<br />
Support Services Minor Change GSSL-MIN-<br />
CJ551-202.<br />
10<strong>01</strong>7125 AIRTOURING LTD <strong>EASA</strong>.R.S.<strong>01</strong>212 AGUSTA A-109 C Installation of Dual GNS430, GTX330 and<br />
PMA700B<br />
10030747 AIRWELD, INC. P-<br />
<strong>EASA</strong>.IM.A.S.03228<br />
10<strong>01</strong>6989 AIRWOLF AEROSPACE L.L.C. <strong>EASA</strong>.IM.R.S.<strong>01</strong>395 FAA STC SR02491CH ROBINSON R22<br />
ROBINSON R44<br />
707-300C SERIES Vapor Cycle Air Conditioning System<br />
Installation (Validation of FAA STCSA5008NM)<br />
Airwolf Rotor Blade Protective Tape.Installation<br />
of a leading edge protective tape for Robinson<br />
R22 and R44 helicopter models according to<br />
FAA STC SR02491CHNote: The<br />
recommendation for approval is given based<br />
on a review performed in accordance with the<br />
Ty<br />
27.11.2007<br />
02.11.2005<br />
The limitations of FAA STC SA5008NM apply Prior to installation of this modification the 14.07.2009<br />
installer must determinethat the<br />
,,interrelationship between this<br />
modification and any otherpreviously<br />
installed ,,modification will introduce no<br />
adverse effectupon the airworthiness of<br />
the product.<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 69/<strong>462</strong><br />
07.02.2008
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