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 />
10035229 ASI INNOVATION T206H ASI-FAM-0002-<strong>01</strong> Installation of Flir MX10 on Limitation to Cessna T206H serial numbers Prior to installation of this modification it 07.06.2<strong>01</strong>1<br />
Cessna T206H.<br />
445 and 446.<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 />
10039405 ASI INNOVATION CESSNA F150L, FA150L ASI-FAM-082-<strong>04</strong> - Installation of EFIS Aspen<br />
EFD 1000 on Cessna 150<br />
10<strong>04</strong>0616 ASI INNOVATION 1. C90, C90A, C90GT, C90GTI<br />
2. B90, E90<br />
10<strong>04</strong>0891 ASI INNOVATION P2006T ASI-0084-03 dated 30 July 2<strong>01</strong>2 - Installation<br />
of removable missionconsole (without<br />
equipments) in the aircraft cabin in place of<br />
passengerseat.<br />
10<strong>04</strong>0999 ASI INNOVATION EMB-135LR Oven installationDescription as per:ASI SDL,<br />
STC Data List ref. ASI-SDL-0087-03, dated<br />
<strong>01</strong>/08/2<strong>01</strong>2.ASI MDL, Master Drawing List ref.<br />
ASI-MDL-0087-<strong>01</strong>, dated <strong>01</strong>/08/2<strong>01</strong>2.ASI<br />
Technical Dossier ref. ASI-TD-0087-02, dated<br />
<strong>01</strong>/08/2<strong>01</strong>2.<br />
10<strong>04</strong>1603 ASI INNOVATION EMB-120ER "P-RNAV Certification"Description as per<br />
documents in "Associated Technical<br />
Documentation".<br />
10<strong>04</strong>1778 ASI INNOVATION EMB-135LR Cabin interior modification.Description as per<br />
Associated Technical Documentation.<br />
The EFD 1000 must not be used as primary Prior to installation of this modification it 02.05.2<strong>01</strong>2<br />
flight and navigation source.Independent and must be determined thatthe<br />
dissimilar instruments must be installed for interrelationship between this modification<br />
primaryindication of attitude, altitude, airspeed, and any other previouslyinstalled<br />
vertical speed, magneticheading and modification and/ or repair will introduce<br />
navigation data, as required for day a no adverse effectupon the airworthiness<br />
of the product.<br />
VHF, UHF and GPS antennas installation This change is applicable to aircraft:-B90 S/N Prior to installation of this modification it 13.07.2<strong>01</strong>2<br />
provisions according to ASImodification no ASI- LJ-318 to LJ-5<strong>01</strong>-C90 S/N LJ-502 to LJ-1062- must be determined thatthe<br />
FAM-0096-00<br />
C90A S/N LJ-1062 to LJ-1726, LJ-1727 to LJ- interrelationship between this modification<br />
1753 and LJ-1755-C90GT S/N LJ-1727, LJ- and any other previouslyinstalled<br />
1754, LJ-1756 and after-C90GTi S/N LJ-1847, modification and/ or repair will introduce<br />
LJ-1853 and after-E90 S/N LW-1 and after no adverse effectupon the airworthiness<br />
of the product.<br />
This STC shall be used only by ASI Innovation. Prior to installation of this modification it <strong>01</strong>.08.2<strong>01</strong>2<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 />
Applicability limited to EMB-135LR S/N 886 Prior to installation of this modification it<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 />
14.08.2<strong>01</strong>2<br />
Applicability restricted to the following S/Ns:<br />
<strong>01</strong>2, <strong>01</strong>3, 027, 158.<br />
None. <strong>01</strong>.10.2<strong>01</strong>2<br />
Applicability limited to EMB-135LR S/N 886. Prior to installation of this modification it<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 />
15.10.2<strong>01</strong>2<br />
10<strong>04</strong>2<strong>04</strong>5 ASI INNOVATION E90 Mast with relay antenna installation None Prior to installation of this modification it<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 />
05.11.2<strong>01</strong>2<br />
10<strong>04</strong>2513 ASI INNOVATION ATR 42-300 Radio Honeywell HF 950 Installation This<br />
modification consists in installing the<br />
Bendix/King KHF950 HF/SSBCommunication<br />
System. This includes mainly the embodiment<br />
of HF antenna,control unit, receiver, amplifier<br />
coupler and electrical protection.<br />
10<strong>01</strong>6994 ASI SERVICES <strong>EASA</strong>.IM.R.S.<strong>01</strong>403 FAA STC SH296NM BELL 206L-1 Installation of a Rolls Royce model 250-C30P Prior to installation of this modification the<br />
engine and associated airframe and tail rotor installer must determine that the<br />
control modifications similar to the Model 206L- interrelationship between this modification and<br />
3. This STC has been classified as “BASIC” by any other previously installed modification<br />
the FAA and has been approved under the will introduce no adverse effect upon the<br />
PTVP.<br />
airworthiness of the product.<br />
This Modification is limited to MSN 148. Prior to installation of this modification it<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 />
05.12.2<strong>01</strong>2<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 84/<strong>462</strong><br />
06.06.2008
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