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>4783 AVIATION DEFENSE SERVICE (AVdef) <strong>EASA</strong>.A.S.02981 FALCON 20 Enhanced Surveillance Mode S Transponder Major change applicaable to aircraft Fan Jet<br />
16.<strong>01</strong>.2008<br />
installation.<br />
Falcon and Falcon 20 serial numbers 076, 103<br />
and 280 equipped with:- Integrated Collins<br />
Proline IV avionics suite.- DFS Elementary<br />
Mode S Transponder as per <strong>EASA</strong>.A.S.00203<br />
STC.- AvDef Minor change <strong>EASA</strong>.A.C.05646<br />
10037677 AVIATION DEFENSE SERVICE (AVdef) FAN JET FALCON BASIC Carriage of ARPEGE pylons onlyThe purpose<br />
of this approval is to clear the carriage of the<br />
ARPEGEpylons only configuration on Falcon<br />
20 S/N 076.<br />
Restricted to Falcon 20 S/N 076 aircraft.As per Prior to installation of this modification it 14.12.2<strong>01</strong>1<br />
AFM Supplement N° SAFM-FALC20 Rev. 17. 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 />
10<strong>04</strong>0822 AVIATION DEFENSE SERVICE (AVdef) FAN JET FALCON BASIC Carriage of PIRATE pylons only.The purpose is Restricted to Falcon 20 S/N 076 aircraft.As per Prior to installation of this modification it 27.07.2<strong>01</strong>2<br />
to clear the carriage of a new configuration of AFM Supplement N° SAFM-FALC20 Rev. 18. must be determined thatthe<br />
underwingstores, dedicated for ferry<br />
interrelationship between this modification<br />
flights without the PIRATE pods.<br />
and any other previouslyinstalled<br />
modification and/ or repair will introduce<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
10034408 AVIATION ENGINEERING AS AS 350 B2 & AS 350 B3 Installation of Electromagnetic Ground Ice<br />
Thickness Sensor<br />
AS350B2 and AS350B3 post mod Eurocopter<br />
SBT 25.00.62<br />
Prior to installation of this modification it <strong>01</strong>.<strong>04</strong>.2<strong>01</strong>1<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 />
10<strong>04</strong>2854 AVIATION ENGINEERING AS AS365 N1, N2, N3 Modification of Helidyne DPL Litter P/N HD365- STC <strong>EASA</strong>.R.S.<strong>01</strong>072 to be installed The approval holder shall fulfil the 20.12.2<strong>01</strong>2<br />
15-1036 Approved under STCLFVS 21E2.003<br />
obligations of Part 21,<br />
(Sweden). Rebuilding of the Helidyne DPL<br />
Paragraph21.A.118. Prior to installation<br />
Litter tofacilitate Aerolite Platform P/N 007-<br />
of this modification it must be determined<br />
0002633-5<strong>01</strong> (EMS Patient Platform).<br />
thatthe interrelationship between this<br />
modification and any other<br />
previouslyinstalled modification and/ or<br />
repa<br />
10<strong>01</strong>5339 AVIATION FABRICATORS / CENTRAL <strong>EASA</strong>.IM.A.S.00389 REV. 2 SEE ATTACHED <strong>EASA</strong><br />
Installation of aft Jump Seat Kits. 1. Installation per the STC Drawing Lists<br />
17.<strong>04</strong>.2008<br />
APPROVED TYP<br />
defined in the AML is limited to aircraft with<br />
Beech factory installed oxygen system for the<br />
jump seat locations. Aircraft configured for<br />
more than 14 total occupants must be<br />
equipped with a 49 cubic foot or gre<br />
10<strong>01</strong>5427 AVIATION FABRICATORS / CENTRAL <strong>EASA</strong>.IM.A.S.<strong>01</strong>160 FAA STC ST00716WI CESSNA 500<br />
CESSNA 5<strong>01</strong><br />
CESSNA 550<br />
CESSNA 551<br />
CESSNA 560<br />
CESSNA 650<br />
CESSNA S550<br />
Installation of Shoulder Harness Kit 22.07.2005<br />
10<strong>01</strong>5577 AVIATION FABRICATORS / CENTRAL <strong>EASA</strong>.IM.A.S.<strong>01</strong>488 REV. 1 FAA STC SA00622WI SEE <strong>EASA</strong> APPROVED MODEL Installation of shoulder harness kit None Prior to installation of this modification it 11.12.2009<br />
LIST<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 />
10<strong>01</strong>5888 AVIATION FABRICATORS / CENTRAL <strong>EASA</strong>.IM.A.S.02007 FAA STC ST<strong>01</strong>262WI CESSNA 650 Installation of a 1, 2 or 3 place side facing<br />
Divan<br />
10<strong>01</strong>5991 AVIATION FABRICATORS / CENTRAL <strong>EASA</strong>.IM.A.S.02145 FAA STC SA4147SW HAWKER 1000<br />
HAWKER 800<br />
HAWKER 800 XP<br />
HAWKER HS 125<br />
Installation of one, two, three & four-place side<br />
facing seat.<br />
Applicable to aircraft serials 650-0023 and<br />
subsequent.This STC approves only the<br />
installation of the parts contained in the<br />
installation documents referenced above. The<br />
requirements foraisle width, passenger oxygen<br />
systems, seats and safety belts, and uph<br />
This STC grants no operational approval to this<br />
installation, that will need to be obtained from<br />
the State of registry for the particular aircraft<br />
involved as defined in JAR OPS1.<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 89/<strong>462</strong><br />
09.<strong>01</strong>.2007<br />
30.10.2006
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