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>4027 SCANDINAVIAN AVIONICS A/S <strong>EASA</strong>.A.S.<strong>01</strong>093 REV. 1 BEECH 1900<br />
1. Installation of Dual Mode S Transponder For installations on or after 31-Jan-2007, this<br />
05.02.2007<br />
BEECH 200C<br />
MST-67A System with ELS capabilities change is limited to the configuration of aircraft<br />
BEECH 300<br />
(installation prior to 31-Jan-2007)2.<br />
/ equipment type as listed underItem 4. in<br />
BEECH 300LW<br />
Installation of Dual Mode S Transponder MST- Engineering Order, Doc. No. 2021128-EO-03,<br />
BEECH B200C<br />
67A System with ELS and EHS capabilities Issue 5, or later approved issue:<br />
BEECH B300<br />
BEECH B300C<br />
(installation on or after 31-Jan-2007)<br />
10<strong>01</strong>4028 SCANDINAVIAN AVIONICS A/S <strong>EASA</strong>.A.S.<strong>01</strong>094 BEECH 200<br />
Installation of Multifunction Display MFD-640 &<br />
11.02.2005<br />
BEECH B200<br />
RP 1008<br />
10<strong>01</strong>4036 SCANDINAVIAN AVIONICS A/S <strong>EASA</strong>.A.S.<strong>01</strong>109 CESSNA 525 Installation of Honeywell KMH 980 Multi-<br />
Hazard Awareness System including TCAS I<br />
and EGPWS (Class B).<br />
11.<strong>04</strong>.2005<br />
10<strong>01</strong>4037 SCANDINAVIAN AVIONICS A/S <strong>EASA</strong>.A.S.<strong>01</strong>110 CESSNA 525 Installation of WX-500 Stormscope System 11.<strong>04</strong>.2005<br />
10<strong>01</strong>4038 SCANDINAVIAN AVIONICS A/S <strong>EASA</strong>.A.S.<strong>01</strong>111 CESSNA 525 Installation of Bendix/King KLN 94 GPS<br />
System.<br />
11.<strong>04</strong>.2005<br />
10<strong>01</strong>4050 SCANDINAVIAN AVIONICS A/S <strong>EASA</strong>.A.S.<strong>01</strong>132 LEARJET 35<br />
Installation of Honywell CAS 67A ACAS/TCAS Certification Basis: applicable requirements of<br />
31.05.2005<br />
LEARJET 35A<br />
II with dual MST-67A Mode S Transponder CS25 plus JAA TGLs No 8 and 13 1.<br />
10<strong>01</strong>4091 SCANDINAVIAN AVIONICS A/S <strong>EASA</strong>.A.S.<strong>01</strong>189 REV. 1 CESSNA 500<br />
CESSNA 550<br />
CESSNA 560<br />
CESSNA S550<br />
10<strong>01</strong>4092 SCANDINAVIAN AVIONICS A/S <strong>EASA</strong>.A.S.<strong>01</strong>190 CESSNA 650 Installation of FreeFlight 21<strong>01</strong> I/O APPROACH<br />
PLUS GPS Navigation System<br />
10<strong>01</strong>4093 SCANDINAVIAN AVIONICS A/S <strong>EASA</strong>.A.S.<strong>01</strong>191 CESSNA 650 Installation of Honeywell CAS 67A TCAS II<br />
System, including Dual MST 67A Mode S<br />
Transponders<br />
10<strong>01</strong>4095 SCANDINAVIAN AVIONICS A/S <strong>EASA</strong>.A.S.<strong>01</strong>193 BAE ATP Installation of Universal Terrain Awareness<br />
Warning System (TAWS)<br />
10<strong>01</strong>4096 SCANDINAVIAN AVIONICS A/S <strong>EASA</strong>.A.S.<strong>01</strong>194 Installation of Universal UNS-1L Flight<br />
Management System<br />
10<strong>01</strong>4111 SCANDINAVIAN AVIONICS A/S <strong>EASA</strong>.A.S.<strong>01</strong>216 BEECH 300<br />
BEECH B300<br />
10<strong>01</strong>4150 SCANDINAVIAN AVIONICS A/S <strong>EASA</strong>.A.S.<strong>01</strong>270 BEECH 200<br />
BEECH 300<br />
BEECH B200<br />
BEECH B300<br />
10<strong>01</strong>4151 SCANDINAVIAN AVIONICS A/S <strong>EASA</strong>.A.S.<strong>01</strong>271 BEECH 200<br />
BEECH 300<br />
BEECH B200<br />
BEECH B300<br />
Installation of Kannad 406 AF ELT 1. 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 />
07.<strong>04</strong>.2005<br />
- 25.08.2005<br />
- 25.08.2005<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 />
Installation of Honeywell CAS 67A<br />
ACAS/TCAS II with Dual MST-67A Mode S<br />
Transponder<br />
EGPWS Installation on Airbus A300/A310 Refer to AFM Supplement Ref. Dc113-0846<br />
Rev B and to Maintenance Planning Document<br />
Supplement DC114-0846-00 rev A.<br />
Installation of Dual GTX 330D Mode S<br />
Transponder System.<br />
10<strong>01</strong>4162 SCANDINAVIAN AVIONICS A/S <strong>EASA</strong>.A.S.<strong>01</strong>294 BAE 125 -800 SERIES Installation of a Rockwell Collins TCAS 4000<br />
with dual TDR-94D Mode S Transponder<br />
10<strong>01</strong>4199 SCANDINAVIAN AVIONICS A/S <strong>EASA</strong>.A.S.<strong>01</strong>349 REV. 1 BEECH 200<br />
BEECH 300<br />
BEECH 300LW<br />
BEECH B200<br />
BEECH B300<br />
Installation of TAWS ST3400 system.Revision<br />
of the AFM Supplement related to a Minor<br />
Change to <strong>EASA</strong>.A.S.<strong>01</strong>349.Installation of<br />
TAWS ST3400 system.Revision of the AFM<br />
Supplement related to a Minor Change to<br />
<strong>EASA</strong>.A.S.<strong>01</strong>349.<br />
10<strong>01</strong>4200 SCANDINAVIAN AVIONICS A/S <strong>EASA</strong>.A.S.<strong>01</strong>350 CESSNA 500 Installation of Honeywell KMH 880 Multi-<br />
Hazard Awareness System<br />
10<strong>01</strong>4226 SCANDINAVIAN AVIONICS A/S <strong>EASA</strong>.A.S.<strong>01</strong>389 CESSNA 300 SERIES<br />
CESSNA 400 SERIES<br />
10<strong>01</strong>4242 SCANDINAVIAN AVIONICS A/S <strong>EASA</strong>.A.S.<strong>01</strong>451 CESSNA 500<br />
CESSNA 550<br />
CESSNA S550<br />
10<strong>01</strong>4245 SCANDINAVIAN AVIONICS A/S <strong>EASA</strong>.A.S.<strong>01</strong>455 CESSNA 300 SERIES<br />
CESSNA 400 SERIES<br />
Installation of GNS 430A/530A<br />
COMM/NAV/GPS Systems<br />
Installation of GPS400 in center panel with<br />
GAD 42 adapter for roll steering<br />
1. 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 />
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.This STC is approved onl<br />
26.07.2005<br />
26.07.2005<br />
30.05.2005<br />
28.<strong>04</strong>.2005<br />
29.06.2005<br />
26.07.2005<br />
26.02.2007<br />
This STC is approved only for the product<br />
02.<strong>01</strong>.2006<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 />
none 20.09.2005<br />
24.<strong>01</strong>.2006<br />
Installation of GTX 330 Mode S Tansponder 20.09.2005<br />
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