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 />
100283<strong>04</strong> KNOTS 2U, LTD. P-<br />
PA-28-151, PA-28-161,<br />
Piper Wing Tips with Landing / Recognition None Prior to installation of this modification it 16.12.2009<br />
<strong>EASA</strong>.IM.A.S.03267<br />
PA-28-181, PA-28-2<strong>01</strong>T, Lights<br />
must be determined thatthe<br />
PA-28-236, PA-28R-2<strong>01</strong><br />
interrelationship between this modification<br />
PA-28-RT-2<strong>01</strong>T, PA-32-3<strong>01</strong><br />
and any other previouslyinstalled<br />
PA-28R-2<strong>01</strong>T, PA-28RT-2<strong>01</strong>,<br />
modification and/ or repair will introduce<br />
PA-32-3<strong>01</strong> T, PA-32R-3<strong>01</strong>,<br />
no adverse effectupon the airworthiness<br />
PA-32R-3<strong>01</strong>T<br />
of the product.<br />
10031230 KNOTS 2U, LTD. LBA EMZ SA1221 FAA SA1217GL 1. PA-32-3<strong>01</strong>FT, PA-32-3<strong>01</strong>XTC<br />
1. PA-32R-3<strong>01</strong>(HP)<br />
1. PA-32R-3<strong>01</strong>T(TC)<br />
2. PA-32-3<strong>01</strong>, PA-32-3<strong>01</strong>T<br />
2. PA-32R-3<strong>01</strong>, PA-32R-3<strong>01</strong>(SP)<br />
10031235 KNOTS 2U, LTD. FAA STC SA1521GL 1. PA-32-3<strong>01</strong>FT, PA-32-3<strong>01</strong>XTC<br />
1. PA-32R-3<strong>01</strong>(HP)<br />
1. PA-32R-3<strong>01</strong>T(TC)<br />
2. PA-32-3<strong>01</strong>, PA-32-3<strong>01</strong>T<br />
2. PA-32R-3<strong>01</strong>, PA-32R-3<strong>01</strong>(SP)<br />
Installation of wing root fairings in accordance<br />
with FAA STC SA1217GL(Revision of LBA<br />
EMZ 1221, issue 1, dated July 20, 20<strong>01</strong>).<br />
Installation of flaps, aileron, flap/fuselage and<br />
stabilator gap sealsin accordance with FAA<br />
STC SA1521GL.<br />
10031236 KNOTS 2U, LTD. LBA EMZ SA1222 FAA SA1195GL 1. PA-32-3<strong>01</strong>FT, PA-32-3<strong>01</strong>XTC Installation of Flap Hinge Fairing seals in<br />
1. PA-32R-3<strong>01</strong>(HP)<br />
accordance with FAA STCSA1195GL<br />
1. PA-32R-3<strong>01</strong>T(TC)<br />
(Revision of LBA EMZ 1222, issue 1, dated<br />
2. PA-32-260, PA-32-300<br />
2. PA-32-3<strong>01</strong>, PA-32-3<strong>01</strong>T<br />
2. PA-32R-300, PA-32RT-300<br />
2. PA-32R-3<strong>01</strong>(SP), PA-32S-300<br />
2. PA-32R-3<strong>01</strong>T(SP), PA-32R-300<br />
2. PA-32RT-300T<br />
July 20, 20<strong>01</strong>).<br />
10<strong>01</strong>4885 KORFF LUFTFAHRT <strong>EASA</strong>.A.S.03113 GROB G 109<br />
GROB G 109 B<br />
10<strong>01</strong>4470 KUERZI AVIONICS AG <strong>EASA</strong>.A.S.02531 LEARJET 60 Installation of SSFDR and MFDAUInstallation<br />
of a Honeywell Solide State Flight Data<br />
Recorder and Teledyne Mini Data Acquisition<br />
Unit in Learjet Model 60<br />
Changes:- at the luggage compartment to be 1. Limted to S/N: 62192. This STC is<br />
used as basis for instruments,- additional cable approved only for the product configuration as<br />
routing in the wings- reinforced attachment defined in the approved design data referred to<br />
points at the lower side of both wings for under in the paragraphs "Description" and<br />
wing pots- reinforcements of the root tips- “Associated Technical Documentation”.<br />
operation with external loa<br />
Compatibility with other aircraft/engine con<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 />
03.08.2<strong>01</strong>0<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 />
03.08.2<strong>01</strong>0<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 />
03.08.2<strong>01</strong>0<br />
This STC is approved only for the product<br />
configuration as defined in the approved design<br />
data referred to in the paragraph "Description".<br />
Compatibility with other aircraft/engine<br />
configurations shall be determined by the<br />
10<strong>01</strong>4482 KUERZI AVIONICS AG <strong>EASA</strong>.A.S.02545 CESSNA 340A Avionic Retrofit<br />
installer.<br />
This STC is approved only for the product<br />
configuration as defined in the approved design<br />
data referred to in the paragraph "Description".<br />
Compatibility with other aircraft/engine<br />
configurations shall be determined by the<br />
installer.<br />
25.<strong>04</strong>.2006<br />
10<strong>01</strong>4569 KUERZI AVIONICS AG <strong>EASA</strong>.A.S.02673 BOMBARDIER DHC-6 SERIES<br />
300<br />
Installation of KMH-880, GPS-400 & KMD-850. Limited to S/N 0841. 13.<strong>04</strong>.2007<br />
10<strong>01</strong>4716 KUERZI AVIONICS AG <strong>EASA</strong>.A.S.02892 PILATUS PC-12/45 Honeywell GNS-XLS FMS InstallationBy<br />
installing a single GNS-XLS Flight<br />
Management System with GPS and DME<br />
sensor.<br />
HB-FPI S/N 551. Valid for this S/N only. 23.<strong>04</strong>.2007<br />
10<strong>01</strong>4806 KUERZI AVIONICS AG <strong>EASA</strong>.A.S.03<strong>01</strong>0 PILATUS PC-12/47 HF 1050 & AFFS Installation by installing a new S/N 795 for initial installation.Approval valid for<br />
22.03.2007<br />
HF-1050 HF COM System with a PS440 HF<br />
Control Panel and a new F5K AFFS<br />
(Automated Flight Following System).<br />
S/N 795 and any other PC-12/47.<br />
10<strong>01</strong>4878 KUERZI AVIONICS AG <strong>EASA</strong>.A.S.03105 PIPER PA-31T Installation of Dual Mode-S XPDR &<br />
TASInstallation of- Dual Mode S Transponder<br />
GTX-330D with diversity antenna.- Traffic<br />
10<strong>01</strong>4945 KUERZI AVIONICS AG <strong>EASA</strong>.A.S.03205 CESSNA 340A<br />
Advisory System SKY497<br />
Installation of a Traffic Advisory System:By<br />
installing a SKY497 Skywatch Traffic Advisory<br />
System with appropriate antenna. Traffic<br />
information will be displayed on<br />
existingsystems.<br />
Reg. HB-LNLS/N: 31T-8020083Valid for this<br />
S/N only<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 300/<strong>462</strong><br />
30.<strong>04</strong>.2007<br />
11.12.2006<br />
11.05.2007<br />
28.08.2007
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