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 />
10036958 SCANDINAVIAN AVIONICS DESIGN<br />
BAE 146, AVRO 146-RJ Provision for a Dual NAVAERO t.BagC2 Class None This STC for the provision for a dual 19.10.2<strong>01</strong>1<br />
GMBH<br />
2 Electronic Flight BagSystem<br />
Class 2 Electronic Flight Bag hasbeen<br />
assessed using the guidance in JAA<br />
Temporary Guidance Leaflet (TGL)No.<br />
36. As part of that airworthiness<br />
assessment a limited evaluationwas<br />
made of the proposed EFB installation o<br />
10037345 SCANDINAVIAN AVIONICS DESIGN<br />
GMBH<br />
10038456 SCANDINAVIAN AVIONICS DESIGN<br />
GMBH<br />
10039000 SCANDINAVIAN AVIONICS DESIGN<br />
GMBH<br />
10<strong>04</strong>0003 SCANDINAVIAN AVIONICS DESIGN<br />
GMBH<br />
10<strong>04</strong><strong>04</strong>72 SCANDINAVIAN AVIONICS DESIGN<br />
GMBH<br />
10<strong>04</strong>0973 SCANDINAVIAN AVIONICS DESIGN<br />
GMBH<br />
10<strong>04</strong>2855 SCANDINAVIAN AVIONICS DESIGN<br />
GMBH<br />
CESSNA 525B Installation of L3 FA2100 Digital FDR S/N 525B-135 and onAccording limitation<br />
section of AFM-S<br />
ATP Installation of a Five Panel Universal EFI-890R<br />
EFIS.<br />
1. 200, 200C, 300, 300LW<br />
2. B200, B200C, B300, B300C<br />
REV. 1 MU-300 (DIAMOND I)<br />
MU-300 (DIAMOND IA)<br />
Installation of Universal UNS FMS System This change is limited to the configuration of<br />
aircraft / equipment typeas listed under<br />
Chapter 4. in <strong>EASA</strong> approved Engineering<br />
Order, Doc. No.2073065-EO, Issue 1, dated<br />
22-Mar-2<strong>01</strong>2, or later approved issue.<br />
B300, B300C Installation of Mission Antennas and a Drop<br />
Tube<br />
10<strong>01</strong>4565 SCHERDEL ENGINEERING Ltd. <strong>EASA</strong>.A.S.02665 Change of Empty Mass and Ballast<br />
Requirements for the Glider LS1-f<br />
10<strong>01</strong>5154 SCHERDEL ENGINEERING Ltd. <strong>EASA</strong>.A.S.03519 DG 400<br />
DG 500 M<br />
DG 600M<br />
DG 800A<br />
SCHEMPP JANUS CM<br />
SCHEMPP NIMBUS 4M<br />
Prior to installation of this modification it 18.11.2<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.If the<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 />
17.02.2<strong>01</strong>2<br />
The installation of this modification by<br />
third persons is subject towritten<br />
permission of the approval holder and<br />
disposal of the approvedappropriate<br />
documentation.Prior to installation of this<br />
modification it must be determined<br />
thatthe interrelationship b<br />
none This STC must be installed in<br />
concurrence with the Scandinavian<br />
AvionicsMinor Changes as referenced in<br />
their Document 2069196-EO.This STC<br />
does not cover Changes in Cabin<br />
Layout.Prior to installation of this<br />
modification it must be determined<br />
thatthe interr<br />
Digital FDR Installation This change is limited to the configuration of<br />
aircraft / equipment typeas listed under<br />
Chapter 4. in <strong>EASA</strong> approved Engineering<br />
Order, Doc. No.2076242-EO, Issue 1, dated<br />
26-June-2<strong>01</strong>2, or later approved issue.<br />
29.03.2<strong>01</strong>2<br />
08.06.2<strong>01</strong>2<br />
The installation of this modification by 09.07.2<strong>01</strong>2<br />
third persons is subject towritten<br />
permission of the approval holder and<br />
disposal of the approvedappropriate<br />
,,documentation.Prior to installation of this<br />
modification it must be determined<br />
thatthe interrelationship<br />
ATP FMS Upgrade for P-RNAV 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 />
10.08.2<strong>01</strong>2<br />
228-200/-2<strong>01</strong>/-202/-212 Installation of GARMIN GTN750 / GTN650 and - This change is limited to the configuration of The installation of this modification by 20.12.2<strong>01</strong>2<br />
Sandel SN4500 EHSI<br />
aircraft and equipmentas defined in the third persons is subject towritten<br />
Engineering Order, Doc. No. 2077918-EO, permission of the approval holder and<br />
Section 4- LNAV/VNAV or LPV is not disposal of the approvedappropriate<br />
permittedIf the holder agrees to permit another documentation.Prior to installation of this<br />
person to use this certificate toalter the p modification it must be determined<br />
thatthe interrelationship b<br />
Alternate fuel lines for Rotax engine powered<br />
glider.<br />
This STC is approved only for the product<br />
configuration as defined in the approved design<br />
data referred to in the paragraphs "Description"<br />
and “Associated Technical Documentation”.<br />
Compatibility with other aircraft/engine<br />
configurations shall be determined<br />
19.02.2007<br />
For all serial numbers. 11.06.2008<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 400/<strong>462</strong>
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