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 />
10039<strong>01</strong>7 SA BERINGER 1<strong>01</strong><br />
BRGAP-STC-003(0) dated 30 Jan 2<strong>01</strong>2 - None. Prior to installation of this modification it 30.03.2<strong>01</strong>2<br />
1<strong>01</strong>A<br />
Replacement of wheel and brakesystem.<br />
must be determined thatthe<br />
1<strong>01</strong>AP<br />
interrelationship between this modification<br />
1<strong>01</strong>B<br />
and any other previouslyinstalled<br />
1<strong>01</strong>BC<br />
modification and/or repair will introduce<br />
1<strong>01</strong>D<br />
no adverse effectupon the airworthiness<br />
1<strong>01</strong>P<br />
of the product.<br />
10<strong>04</strong>1414 SA BERINGER REV. 1 ASW 20 BL,ASW 20 C,ASW 20 BRGAP-STC-005(0) - Replacement of wheel<br />
CL<br />
ASW 20 F,ASW 20 FL,ASW 20 B<br />
ASW 20,ASW 20 L<br />
and brake system<br />
10<strong>04</strong>1955 SA BERINGER DR400-100/-120/-120A/-120D/125<br />
DR400-125I/-140/-140B/-160/<br />
DR400-160D/-180/-180R/-180S<br />
DR400-200R/-2+2/-500/-NGL/-RP<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 />
19.09.2<strong>01</strong>2<br />
BRGAP-STC-006 - Replacement of brake unit. 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 airwOr1hiness<br />
of the product.<br />
26.10.2<strong>01</strong>2<br />
10<strong>01</strong>4488 SAAB AB <strong>EASA</strong>.A.S.02550 BEECH A100 Installation of avionics in accordance with Saab This STC is limited to Beech A100, s/n B-217<br />
Aerotech AB, TDM06-<strong>04</strong><br />
19.<strong>04</strong>.2006<br />
10<strong>01</strong>4508 SAAB AB <strong>EASA</strong>.A.S.02582 LEARJET 35A Mission Power -- 20.06.2006<br />
10<strong>01</strong>4936 SAAB AB <strong>EASA</strong>.A.S.03192 CESSNA 560 Replacement of SSR Mode S Transponders<br />
for compliance with Enhanced Surveillance.<br />
<strong>04</strong>.12.2007<br />
10<strong>01</strong>4937 SAAB AB <strong>EASA</strong>.A.S.03193 CESSNA 650 Replacement of SSR Mode S Transponders<br />
for compliance with Enhanced Surveillance.<br />
<strong>04</strong>.12.2007<br />
10<strong>01</strong>5123 SAAB AB <strong>EASA</strong>.A.S.03472 MITSUBISHI MU-2B Garmin GTX 330/330D (SSR Mode S<br />
Transponder) upgrades for compliance with<br />
Enhanced Surveillance (EHS) requirements.<br />
27.03.2008<br />
10<strong>01</strong>5162 SAAB AB <strong>EASA</strong>.A.S.03532 LEARJET 35A Mode S Enhanced Surveillance (EHS)<br />
Upgrade.<br />
EHS Non Capable. <strong>01</strong>.07.2008<br />
10029935 SAAB AB MU-2B Installation Provisions/Video Signal in Mitsubishi Target Towing provisions according to Swedish Prior to installation of this modification it <strong>04</strong>.05.2<strong>01</strong>0<br />
MU-2B rear pressurebulkhead<br />
CAA approval C6A/71 mustbe installed. 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 />
10031209 SAAB AB P-<strong>EASA</strong>.A.S.03618 REV. 2 382 Installation of Saab Missile Protection System.<br />
The installationconsists of a forward sensor<br />
fairing on both sides of the nose and arear<br />
sensor installation in the tail. The dispensers<br />
are installed onboth sides under the rear edge<br />
of the wing.Inside the a<br />
Aircraft Serial 4954 Only The STC grants no operational approval,<br />
the aircraft operator will needto obtain<br />
operational approval from the Agency or<br />
Authority responsiblefrom the State of<br />
registry and the State in whose airspace<br />
it is to beoperated.Prior to installation of<br />
this modif<br />
10033697 SAAB AB AS 355 E, AS 355 F, AS 355 F1 Installation of New TopEye Mission Box none Prior to installation of this modification it 03.02.2<strong>01</strong>1<br />
AS 355 F2, AS 355 N, AS 355 NP<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 />
10038972 SAAB AB C-212-EE TDM10-05 Rev. G titled "Cabin Layout", dated<br />
2<strong>01</strong>2-03-20."New Cabin Layout for Maritime<br />
Surveillance System in CASA<br />
C212".Installation and Mounting of Maritime<br />
Surveillance System and change ofCabin<br />
Layout to accommodate a maximum of 5 crew<br />
members and nopa<br />
All equipment necessary for Maritime<br />
Surveillance Missions shall beinstalled or<br />
added with <strong>EASA</strong> DOA 21J.108 Minor Change<br />
Approvals<br />
21.12.2<strong>01</strong>0<br />
Prior to installation of this modification it 27.03.2<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 />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 388/<strong>462</strong>
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