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 />
10036439 AVCON INDUSTRIES, Inc. FAA STC SA0<strong>04</strong>15WI 100, A100, A100A, A100C, B100 Installation of Baggage Door. None Prior to installation of this modification it 08.09.2<strong>01</strong>1<br />
200, 200T, A200, B200, B200T<br />
must be determined thatthe<br />
300, 300LW, B300<br />
interrelationship between this modification<br />
B90, C90, C90A, E90, H90<br />
and any other previouslyinstalled<br />
modification and/ or repair will introduce<br />
no adverse effectupon the airworthiness<br />
of the product<br />
10<strong>01</strong>6623 AVIATION CONSULTING &<br />
ENGINEERING<br />
<strong>EASA</strong>.IM.A.S.03054 FAA STC SA<strong>01</strong>282WI CESSNA 525 Installation of Replacement of Seat Cushions. 1. 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.2.<br />
10<strong>01</strong>4067 AVIATION DEFENSE SERVICE (AVdef) <strong>EASA</strong>.A.S.<strong>01</strong>154 REV. 2 BEECH 200<br />
BEECH B200<br />
10<strong>01</strong>4068 AVIATION DEFENSE SERVICE (AVdef) <strong>EASA</strong>.A.S.<strong>01</strong>155 BEECH 200<br />
BEECH B200<br />
Installation of an Emergency Locator ELT 96 -<br />
406 MhZ.<br />
Installation of 2 Mode S transponders MST<br />
67A.<br />
This STC is limited to Beechcraft 200 MSN BB<br />
199, Beechcraft B200 MSN BB920 and<br />
Beechcraft 200 s/n BB439.<br />
1. This STC requires a pre-modification: 2<br />
bottom transponder antennas.2. This STC is<br />
limited to Beech s/n BB199 and Beech 200 s/n<br />
BB439.<br />
This STC is limited to Beechcraft C90 s/n<br />
LJ860 and Beechcraft E90 s/n LW251.<br />
10<strong>01</strong>4069 AVIATION DEFENSE SERVICE (AVdef) <strong>EASA</strong>.A.S.<strong>01</strong>157 BEECH C90<br />
Installation of an Emergency Locator ELT 96-<br />
BEECH E90<br />
406 MhZ.<br />
10<strong>01</strong>4070 AVIATION DEFENSE SERVICE (AVdef) <strong>EASA</strong>.A.S.<strong>01</strong>158 BEECH C90 Installation of Mode S Transponder MST 67A. 1. This STC requires a pre-modification: 2<br />
bottom transponders antennas.2. This<br />
Modification is limited to Beechcraft C90 s/n<br />
LJ860.<br />
10<strong>01</strong>4146 AVIATION DEFENSE SERVICE (AVdef) <strong>EASA</strong>.A.S.<strong>01</strong>265 BEECH C90 Replacement of Primus 40 weather radar by a This STC is limited to Beechcraft C90 s/n<br />
Primus weather Radar.<br />
LJ860.<br />
10<strong>01</strong>4212 AVIATION DEFENSE SERVICE (AVdef) <strong>EASA</strong>.A.S.<strong>01</strong>370 BEECH 58 Installation of emergency locator transmitter Modification limited to s/n TH-647The AFMS<br />
ELT 96-406 MHz in accordance with<br />
No. 1 / AvDef Beech 58 must be used with this<br />
modification file AVD-MB58-23-<strong>04</strong>4A. modification.<br />
10<strong>01</strong>4584 AVIATION DEFENSE SERVICE (AVdef) <strong>EASA</strong>.A.S.02691 REV. 1 FALCON 20<br />
AVD-MDA20-95-054B: Installation of new age 1. Limitations iaw SAFM FALC20 apply for<br />
FAN JET<br />
Alkan Pylon6075(76)C006<br />
operation with AVDMDA20-95-054B2. Prior to<br />
installation of this modification the installer must<br />
determine that the interrelationship between<br />
this modification andany other previously<br />
installed modification will intr<br />
10<strong>01</strong>4585 AVIATION DEFENSE SERVICE (AVdef) <strong>EASA</strong>.A.S.02692 MYSTERE FALCON 20 AVD-MDA20-95-055A: Installation of underwing<br />
stores<br />
10<strong>01</strong>4586 AVIATION DEFENSE SERVICE (AVdef) <strong>EASA</strong>.A.S.02693 MYSTERE FALCON 20-C5<br />
MYSTERE FALCON 20-D5<br />
MYSTERE FALCON 20-E5<br />
STRUCTURAL INSTALLATION OF A FUGRO<br />
GPS ANTENNA ON THE FUSELAGE<br />
1. Limitations iaw AFM Supplement SAFM-<br />
FALC20 to DTM 918 apply for operation with<br />
POD installation iaw AVD-MDA20-95-055A2.<br />
Prior to installation of this modification the<br />
installer must determine that the<br />
interrelationship between this modification<br />
andany o<br />
Compatibility with previous approved<br />
modifications shall be determined by the<br />
installer.<br />
10<strong>01</strong>4587 AVIATION DEFENSE SERVICE (AVdef) <strong>EASA</strong>.A.S.02694 MYSTERE FALCON 20 AVD-MDA20-25-050A: Installation of consoles<br />
in cabin.<br />
10<strong>01</strong>4639 AVIATION DEFENSE SERVICE (AVdef) <strong>EASA</strong>.A.S.02785 MYSTERE FALCON 20 AVD-MDA20-49-053A: Additional Power Bus Limitations iaw AFM supplement to DTM 918 -<br />
using APU generation, installation of 2 AFMS FA20 apply for operation with additional<br />
additional inverters.<br />
inverters installed iaw AVD-MDA20-49-053A.<br />
10<strong>01</strong>4724 AVIATION DEFENSE SERVICE (AVdef) <strong>EASA</strong>.A.S.029<strong>01</strong> FALCON 10 AVD-MDA10-34-060A: installation of EGPWS<br />
Mark VIII<br />
10<strong>01</strong>4730 AVIATION DEFENSE SERVICE (AVdef) <strong>EASA</strong>.A.S.02909 REV. 1 FALCON 20 AVD-MDA20-95-057A: Activation of the SETHI<br />
2 missionAVD-MDA20-95-054B: RAMHY<br />
Project - VHF/UHF Atenna<br />
Limitations iaw AFM Supplement Supavd1 to<br />
DTM 721 apply for operation with EGPWS<br />
installation iaw AVD-MDA10-34-060A.TGL 12<br />
complied with.Cert basis FAR 25 Amdt 20.<br />
1. This STC ensures proper isolation of<br />
Payload (SETHI Mission Equipment) from /<br />
return to - civil configuration in case of<br />
inadvertent activation.2. Activated SETHI<br />
Mission Equipment is not approved by<br />
<strong>EASA</strong>.3. Limitations iaw AFM Supplement<br />
10<strong>01</strong>4760 AVIATION DEFENSE SERVICE (AVdef) <strong>EASA</strong>.A.S.02950 BEECH 200 Installation of two 8.33 kHz VHF<br />
SAFM-FALC20 to<br />
This STC is limited to the S/N BB199 and<br />
BB920<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 88/<strong>462</strong><br />
03.12.2008<br />
15.03.2005<br />
28.07.2005<br />
28.07.2005<br />
22.07.2005<br />
28.07.2005<br />
21.<strong>04</strong>.2006<br />
24.11.2008<br />
24.11.2008<br />
23.<strong>04</strong>.2007<br />
15.11.2007<br />
10.<strong>01</strong>.2008<br />
26.11.2007<br />
18.12.2008<br />
<strong>04</strong>.<strong>04</strong>.2007
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