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>4939 S.E.A.M. <strong>EASA</strong>.A.S.03196 PIPER PA-23-250 Modification d'installation Radio/Couplage B-<br />
RNAV.Dépose: 2KX 175B+1 B.A. KMA 20+1<br />
ADF KR85 + 1DLE KN65 + 1GPS 155XL +<br />
1ATC KT 76 A.Pose: 1GNS 430 + 1KX 155 +<br />
1B.Q. GMA 340 +1 ADF KR 87 + 1 DME KN<br />
62A + 1 ATC GTX 330 + 1 MD41.<br />
Limited to S/N 27-4727 F-GOPR. 07.11.2007<br />
10<strong>01</strong>4944 S.E.A.M. <strong>EASA</strong>.A.S.03202 REV. 1 PIPER PA-28R-2<strong>01</strong>T Installation modification B-RNAV.Installation of<br />
annunciation unit Mid Continent MD 41-1484.<br />
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 install<br />
10<strong>01</strong>4970 S.E.A.M. <strong>EASA</strong>.A.S.03250 BEECH F90 Transponder ATC GTX330D, Radio/GPS GNS Modification limited to SN LA-19.AFMS 1609-<br />
530 and Radio/GPS GNS 430 installation. 07-<strong>01</strong>, 1609-07-02 and 1609-07-03 must be on<br />
board.<br />
10<strong>01</strong>5070 S.E.A.M. <strong>EASA</strong>.A.S.03396 PIPER PA-28R-200 Modification d'installation Radio / B-RNAV sans 1. Prior to installation of this modification the<br />
couplage PADépose: 1 boite audio KA 134+1 installer must determine that the<br />
GPS 150XL+1 VHF/VOR KX 155 + IND KI interrelationship between this modification<br />
208 + 1MKRKR21 + 1 ATC KT 76APose: 1 andany other previously installed modification<br />
boite audio/MKR GMA 340 + 1<br />
will introduce no adverse effect upon the<br />
VHF/VOR/GLD/GPS GNS 430 + IND GI airworthiness of the product.2. The ins<br />
10<strong>01</strong>5095 S.E.A.M. <strong>EASA</strong>.A.S.03432 CESSNA 210E STC 1862-08 - Avionic modification for<br />
BRNAV navigation and autopilot coupling.<br />
10<strong>01</strong>5105 S.E.A.M. <strong>EASA</strong>.A.S.03448 SOCATA TB 20 Installation of a GNS 430 W for IFR B-RNAV<br />
"en route" operations, without coupling to<br />
automatic pilot.<br />
07.10.2008<br />
21.09.2007<br />
02.03.2009<br />
Limited to S/N 58625. 29.<strong>04</strong>.2008<br />
1. This installation is limited to TB 20 s/n<br />
791.2. Prior to installation of this modification<br />
the installer must determine that the<br />
interrelationship between this modification and<br />
any other previously installed modification will<br />
introduce no adverse<br />
10<strong>01</strong>5135 S.E.A.M. <strong>EASA</strong>.A.S.03488 BEECH 58 STC 1940-08- Avionic modification for BRNAV Limitation to s/n TH 14<strong>01</strong><br />
navigation and autopilot coupling.<br />
06.05.2008<br />
10<strong>01</strong>5196 S.E.A.M. <strong>EASA</strong>.A.S.03582 PIPER PA-44-180 Modification d'installation B-RNAV : pose L’installation de ce STC est limitée au PA44-<br />
30.09.2008<br />
Annonciateur DWA 1000<br />
180 S/N 4479953081 L'utilisation du GPS en<br />
approche et sur SID's et STAR est interdite1<br />
Pré-requis: FAM 20<strong>04</strong>/08 “Pose GNS 430”<br />
suivant la modification approuvée<br />
<strong>EASA</strong>.A.C.096471 Avant installation de ce<br />
10<strong>01</strong>5214 S.E.A.M. <strong>EASA</strong>.A.S.03629 BEECH 200 Modification d'installation transpondeur Mode<br />
S: dépose 2 transpondeurs KXP 755 + Boite<br />
de commande + 2 antennes ATC / Pose 2<br />
transpondeurs GTX 330D + 4 antennes ATC<br />
1. This modification is valid only for aircraft<br />
Beech 200, S/N BB 406.2.2. Prior to<br />
installation of this modification the installer must<br />
determine that the interrelationship between<br />
this modification and any other previously<br />
installed modification wi<br />
10<strong>01</strong>5243 S.E.A.M. <strong>EASA</strong>.A.S.03678 CESSNA 182R MODIFICATION D'INSTALLATION B-RNAV<br />
avec couplage au pilote automatique<br />
Limitation to Cessna 182R S/N 182-68316 30.03.2009<br />
10029007 S.E.A.M. BEECH 58P STC 2589/09 - Radio B-RNAV avec couplage Limited to: S/N TJ-74 Prior to installation of this modification it 25.02.2<strong>01</strong>0<br />
PA<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 />
10032905 S.E.A.M. PA-28RT, PA-2<strong>01</strong>T, Avionic modification: dual installation of Garmin<br />
GNS 430W (with GA 35antennas) for B-RNAV<br />
operation with coupling to autopilot,<br />
installationof GMA 340 audio Intercom, KN 62A<br />
DME receiver and WX 500 stormsocpewith<br />
NY163 antenna<br />
17.<strong>04</strong>.2009<br />
05.08.2008<br />
The installation is limited to aircraft PA- Prior to installation of this modification it 07.12.2<strong>01</strong>0<br />
28RT/PA-28T S/N 28R813143.The aircraft must be determined thatthe<br />
must be equipped with a third radionavigation interrelationship between this modification<br />
orradiocommunicator mean independent from and any other previouslyinstalled<br />
the two GNS 430 units.The GNS 430W modification and/ or repair will introduce<br />
software version must be No 3.3. Installation of no adverse effectupon the airworthiness<br />
a<br />
of the product.<br />
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