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 />
10034238 BUSINESS & COMMUTER AIRCRAFT 1900C, 1900D BCA 120 revision 0 - 28-230 volts inverter(s) Not applicable Prior to installation of this modification it 17.03.2<strong>01</strong>1<br />
Installation on Beech 1900Series.<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 />
1003<strong>462</strong>2 BUSINESS & COMMUTER AIRCRAFT BEECH 1900D BCA 85 rev 3 - Full VIP Cabin Installation<br />
Beech 1900D<br />
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 />
18.<strong>04</strong>.2<strong>01</strong>1<br />
10035661 BUSINESS & COMMUTER AIRCRAFT B200 Installation of a ADF60 on a Beech 200 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 />
08.07.2<strong>01</strong>1<br />
10035662 BUSINESS & COMMUTER AIRCRAFT B200 Installation of a ALT4000 on a Beech 200 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 />
08.07.2<strong>01</strong>1<br />
10035665 BUSINESS & COMMUTER AIRCRAFT B200 Installation of a DME4000 on a Beech 200 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 />
08.07.2<strong>01</strong>1<br />
10038717 BUSINESS & COMMUTER AIRCRAFT <strong>EASA</strong>.A.S.00327 REV. 1 B1900D Installation of Two Transponders mode S RCZ- BEECH 1900 D S/N UE 70 The approval holder shall fulfil the 09.03.2<strong>01</strong>2<br />
852<br />
obligations of Part<br />
21,Paragraph21.A109.Prior to installation<br />
of this modification it must be determined<br />
thatthe interrelationship between this and<br />
any other previously installedand/ or<br />
repair will introduce no adverse<br />
10<strong>01</strong>6240 BUTLER NATIONAL CORPORATION <strong>EASA</strong>.IM.A.S.02512 FAA STC NO. ST00846SE BOEING 747-100<br />
BOEING 747-200<br />
BOEING 747-300<br />
10<strong>01</strong>6460 BUTTERFIELD INDUSTRIES, INC. <strong>EASA</strong>.IM.A.S.02806 FAA STC SA4362NM BEECH 200<br />
BEECH B200 SERIES<br />
Installation of Model 840037-108, 840037-112, This STC is approved only for the product<br />
and 840037-113 transient Suppression Device configuration as defined in the approved design<br />
on Boeing 747-100, 747-200, 747-300 SP and data. Compatibility with other aicraft/engine<br />
SR series airplanes fitted with Honeywell configuraitons shall be determined by the<br />
Analog Fuel quantity Indication System in installer.<br />
accordance with Butler National Corpora<br />
Installation of Butterfield Industries Oil Residue<br />
Collection System Kit P/N BI 1<strong>01</strong>1-1<br />
10<strong>01</strong>6461 BUTTERFIELD INDUSTRIES, INC. <strong>EASA</strong>.IM.A.S.02807 FAA STC SA00829CH BEECH B200 SERIES Installation of Butterfield Industries Air/Oil<br />
Separator System Kit P/N BI 60<strong>01</strong>-1<br />
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<br />
will introduce no adverse effect upon the<br />
airworthiness of the prod<br />
Aircraft which are not modified by STC<br />
SA4362NM, will also require installation of an<br />
oil collection tank1 Prior to installation of this<br />
modification the installer must determine that<br />
the interrelationship between this<br />
modification and any other pre<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 149/<strong>462</strong><br />
15.10.2007<br />
08.08.2008<br />
08.08.2008
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