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>5111 BUSINESS & COMMUTER AIRCRAFT <strong>EASA</strong>.A.S.03454 REV. 1 BEECH BARON 58 Dual Garmin Installation : GNS-530 (GPS Airplane Flight Manual Supplement ref. BCA<br />
08.05.2008<br />
approaches and PRNAV approved) + GNS 107-06, revision 2, dated 23 April 2008 or later<br />
430 on Baron 58 (EFS 40/50 equipped). approved revision must be used when<br />
modification is applied in the<br />
Aircraft.Modification limited to s/n TH-1510, TH-<br />
1515, TH-1537, TH-17<strong>01</strong> to TH-1706, TH-<br />
1734 and T<br />
10<strong>01</strong>5140 BUSINESS & COMMUTER AIRCRAFT <strong>EASA</strong>.A.S.03496 DGAC AAC NO. 751 BEECH 1900C, AIRLINER Installation of a King/ Bendix KLN-90B GPS 1. The supplemental AFM No. TF524PA<br />
28.02.2008<br />
with B-RNAV capacity.Note: This STC revises must be used when the modification is<br />
DGAC approval AAC No. 751.<br />
installed.2. Limited to S/N UC-168, F-GVLC<br />
and UC-153, F-GNPM.<br />
10<strong>01</strong>5232 BUSINESS & COMMUTER AIRCRAFT <strong>EASA</strong>.A.S.03655 BEECH 200<br />
Be ‘Mode S / Flight ID’ capable Collins TDR- Prior to installation of this modification the<br />
27.<strong>04</strong>.2009<br />
BEECH 300<br />
94(D) transponders.<br />
installer must determine that the<br />
BEECH B200<br />
interrelationship between this modification and<br />
BEECH B300<br />
any other previously installed modification will<br />
introduce no adverse effect upon the<br />
airworthiness of the product.<br />
10<strong>01</strong>5239 BUSINESS & COMMUTER AIRCRAFT <strong>EASA</strong>.A.S.03666 BEECH C90<br />
BCA 110 Rev. 3 - Garmin GNS-x30WA (GNS- Prior to installation of this modification the<br />
09.<strong>01</strong>.2009<br />
BEECH C90A<br />
530WA or GNS-430WA) and Sandel SN4500 installer must determine that the<br />
BEECH E90<br />
installation for B-RNAV, P-RNAV and GNSS interrelationship between this modification and<br />
BEECH F90<br />
approaches.<br />
any other previously installed modification<br />
will introduce no adverse effect upon the<br />
airworthiness of the product.<br />
10<strong>01</strong>5291 BUSINESS & COMMUTER AIRCRAFT <strong>EASA</strong>.A.S.03830 REV. 1 200C BCA112 revision 2, dated 15 July 2<strong>01</strong>2 : Limitation to sn BB-1473 Prior to installation of this modification it 25.07.2<strong>01</strong>2<br />
underwings, rooftop and PODantennas<br />
must be determined thatthe<br />
installation and belly antennas relocation.Major<br />
interrelationship between this modification<br />
Change of STC <strong>EASA</strong>.A.S.03830.<br />
and any other previouslyinstalled<br />
modification and/or repair will introduce<br />
no adverse effectupon the airworthiness<br />
of the product. The app<br />
10<strong>01</strong>5307 BUSINESS & COMMUTER AIRCRAFT <strong>EASA</strong>.A.S.03899 BEECH B90<br />
BEECH C90<br />
BEECH E90<br />
Be ‘Mode S / Flight ID’ capable Collins TDR-<br />
94(D) transponders.<br />
10<strong>01</strong>5308 BUSINESS & COMMUTER AIRCRAFT <strong>EASA</strong>.A.S.03900 BEECH F90 Be ‘Mode S / Flight ID’ capable Collins TDR-<br />
94(D) transponders.<br />
10027323 BUSINESS & COMMUTER AIRCRAFT B300 HF-9000 installation on Beech B300 Series<br />
PROLINE 21 Equipped<br />
10029562 BUSINESS & COMMUTER AIRCRAFT BEECH C90A BCA117 rev 0 - GPS replacement and aircraft<br />
capacity validation forB-RNAV, P-RNAV and<br />
GNSS approaches prodecures<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 will<br />
introduce no adverse effect upon the<br />
airworthiness of the product.<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 will<br />
introduce no adverse effect upon the<br />
airworthiness of the product.<br />
Modification applicable to B300 equipped with<br />
Proline 21, serial numberFL-1 and after and<br />
FM-1 and after<br />
27.<strong>04</strong>.2009<br />
27.<strong>04</strong>.2009<br />
1) The approval holder shall fulfil the 21.09.2009<br />
obligations of Part 21,Paragraph<br />
21.A1092) Prior to installation of this<br />
modification it must be determined<br />
thatthe interrelationship between this<br />
modification and any other<br />
previouslyinstalled modification and/or re<br />
Limited to: S/N LJ-1660 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 />
<strong>01</strong>.<strong>04</strong>.2<strong>01</strong>0<br />
10032469 BUSINESS & COMMUTER AIRCRAFT C90 BCA118-00 - ADF system upgrade on beech<br />
S/N LJ - 894<br />
Limitation to beech C90 SN LJ-894 09.11.2<strong>01</strong>0<br />
10034237 BUSINESS & COMMUTER AIRCRAFT REV. 1 1900D Double GARMIN GPS400W Installation for B- Installation limited to Beech 1900D equipped Prior to installation of this modification it 15.06.2<strong>01</strong>2<br />
RNAV and P-RNAV and RNPApproach LNAV with Rockwell CollinsAPC-65H autopilot or must be determined thatthe<br />
procedures, according to modification No BCA FYD-65 H flight director and EFIS Rockwell interrelationship between this modification<br />
121.Revision 1 adding the coupling to Rockwell CollinsDPU 84, upgraded for GPS approach and any other previouslyinstalled<br />
Collins FYD-65 H flightdirector.<br />
through Rockwell Collins SB 77(523-0805196) modification and/ or repair will introduce<br />
and SB 81 (523-0805<strong>04</strong>6).<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 148/<strong>462</strong>
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