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
10015052 SCANDINAVIAN AVIONICS A/S EASA.A.S.03373 DE HAVILLAND CANADA DHC6- Dual Directional Gyro, Dual EHSI/RMI and As detailed in the AFM 2043963-AM 05.03.2008
300
DE HAVILLAND DHC6-310
audio System.
10015057 SCANDINAVIAN AVIONICS A/S EASA.A.S.03379 BEECH 200
Installation of Garmin GWX 68 / Garmin GMX This change is limited to the configuration of
30.01.2008
BEECH 200C
200 Weather Radar System.
aircraft / equipment type as listed under Item
BEECH 300
4. of EASA approved Engineering Order, Doc.
BEECH 300LW
No. 2038539-EO, Issue 3, dated 24-Jan-2008
BEECH B200
or later approved issue. The system is not
BEECH B200C
BEECH B300
BEECH B300C
approved for operati
10015061 SCANDINAVIAN AVIONICS A/S EASA.A.S.03384 BEECH 200
Installation of Garmin GPS 500 System This change is limited to the configuration of
30.01.2008
BEECH 200C
(including compliance with AMC 20-4, AMC 20- aircraft / equipment type as listed under Item
BEECH 300
5 and FAA AC20-138A)
4. of EASA approved Engineering Order, Doc.
BEECH 300LW
No. 2038540-EO, Issue 2, dated 22-Jan-2008
BEECH B200
or later approved issue. The system is not
BEECH B200C
BEECH B300
BEECH B300C
approved for operati
10015063 SCANDINAVIAN AVIONICS A/S EASA.A.S.03389 Sandel ST3400 TAWS Installation. 30.05.2008
10015067 SCANDINAVIAN AVIONICS A/S EASA.A.S.03393 CESSNA 500, CITATION Installation of Honeywell ART2100/KMD850 1. This STC is exclusively applicable for
12.03.2008
CESSNA 550 CITATION II Weather Radar System.
aircraft which have the equipment listed in
CESSNA S550, (CITIATION S/II)
chapter 4 of the Scandinavian Avionics
Engineering Order 2044352-EO Issue 2
already installed;2. Prior to installation of this
modification the installer must deter
10015089 SCANDINAVIAN AVIONICS A/S EASA.A.S.03424 FALCON 10 Dual TDR-94D Transponder Upgrade to Previous required aircraft configuration:•
22.02.2008
provide limited Enhanced Surveillance Aircraft equipped with Dual TDR-94D (-007/-
Transponder Mode S capability (Non EHS 008) and installation compliant with Elementary
Capable).
Mode S requisites.• Mode S Transponder
Antenna Diversity• Collins TCAS II System•
Dual ADC’s installation with
10015113 SCANDINAVIAN AVIONICS A/S EASA.A.S.03460 FAN JET FALCON SERIES C
FAN JET FALCON SERIES D
FAN JET FALCON SERIES E
FAN JET FALCON SERIES F
FAN JET FALCON SERIES G
MYSTERE FALCON 20-C5
MYSTERE FALCON 20-D5
MYSTERE FALCON 20-E5
MYSTERE FALCON 20-F5
MYSTERE FALCON 200
10015128 SCANDINAVIAN AVIONICS A/S EASA.A.S.03479 BOMBARDIER DHC-6 SERIES
300
10015131 SCANDINAVIAN AVIONICS A/S EASA.A.S.03482 BEECH 300
BEECH 300LW
BEECH B300
BEECH B300C
10015132 SCANDINAVIAN AVIONICS A/S EASA.A.S.03483 BEECH 200
BEECH 200C
BEECH 300
BEECH 300LW
BEECH B200
BEECH B200C
BEECH B300
BEECH B300C
Dual TDR-94D Transponder Installation
Upgrade to provide both Elementary and
Enhanced Surveillance Transponder Mode S
Capabilities.
Honeywell EGPWS MK VI, TRA-45 Display
installation.
Installation of an L3 F-1000 Digital Flight Data
Recorder System
Installation of a Universal CVR-30B or CVR-
120 Cockpit Voice Recorder
10015137 SCANDINAVIAN AVIONICS A/S EASA.A.S.03490 CESSNA 650 CITATION VII UPGRADE of existing FMS Universal UNS-
1Csp to UNS-1Csp+ to comply with P-RNAV
requirements.
10015170 SCANDINAVIAN AVIONICS A/S EASA.A.S.03544 BEECH 400
BEECH 400A
Mode S ELS/EHS Upgrade of existing
transponder system.
Previous required aircraft configuration:•
Aircraft equipped with Dual TDR-94D
installation with Mode S Diversity Antenna
installation and Radio Tuning Unit RTU-4220•
ADC’s with ARINC 429 Interface.• Collins
TCAS II System• Collins Proline 4 Av
This change is limited to the configuration of
aircraft / equipment type as listed under Item
4. of EASA approved Engineering Order, Doc.
No. 2045502-EO, Issue 2, dated 24-Apr-2008
or later approved issue.
This change is limited to the configuration of
aircraft / equipment type as listed under Item
4. of EASA approved Engineering Order, Doc.
No. 2045503-EO, Issue 2, dated 23-Apr-2008
or later approved issue.
1. 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 i
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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09.06.2008
28.03.2008
05.05.2008
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25.08.2008
10.06.2008