04/01/2013 Page 1/462 - EASA

EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue
10014973 SCANDINAVIAN AVIONICS DESIGN EASA.A.S.03259 REV. 5 737-300, -400, -500, -600 Installation of a Dual navAero Electronic and Not Applicable Prior to installation of this modification it 14.11.2011
GMBH
737-700, -800, -900
logging display system.Change consisting in
must be determined thatthe
installing a dual portable Class 2 EFB's
interrelationship between this modification
t.BagC2system
and any other previouslyinstalled
modification and / or repair will introduce
no adverse effectupon the airworthiness
of the product.
10015305 SCANDINAVIAN AVIONICS DESIGN
GMBH
10026864 SCANDINAVIAN AVIONICS DESIGN
GMBH
10027014 SCANDINAVIAN AVIONICS DESIGN
GMBH
10028068 SCANDINAVIAN AVIONICS DESIGN
GMBH
10028206 SCANDINAVIAN AVIONICS DESIGN
GMBH
10028452 SCANDINAVIAN AVIONICS DESIGN
GMBH
10031128 SCANDINAVIAN AVIONICS DESIGN
GMBH
10031822 SCANDINAVIAN AVIONICS DESIGN
GMBH
EASA.A.S.03894 REV. 1 1. 200, 200C, 300, 300LW
2. B200, B200C, B300, B300C
P-EASA.A.S.03938 REV. 1 CESSNA 500, 550 GARMIN GPS 400W/500W installation
Revision 1 supersedes the previous issue of
this STC to delete the modelS550 from the
applicability list for correction.
P-EASA.A.S.03849 500 (CITATION AND CITATION I) Installation of Honeywell MST 67A Dual Mode
S XPDR transponder.
Dual TDR-94D Mode S ELS/EHS Transponder This change is limited to the configuration of
System Upgrade, and optional forADS-B aircraft / equipment typeas listed under
Chapter 4. in EASA approved Engineering
Order, Doc. No.2073065-EO, Issue 1, dated
22-Mar-2012, or later approved issue
forinstallations without ADS-B, or Issue 2,
dated
P-EASA.A.S.03732 650 (CITATION VII) Software upgrade of installed Honeywell GNS-
XL or GNX-XLS FMS system forP-RNAV
operation
P-EASA.R.S.01586 R22 BETA Title: Camera with supportDescription: Optional
Installation of a camera turret, related
recorderand data link transmitter system in
accordance with Master Document
List2053852 DOC issue 2, dated 04.12.2009.
The installation is based onScandinavian
Avionic
P-EASA.R.S.01580 REV. 1 EC 120 B Replacement of existing SAFT Ni-Cad. battery
with Concorde lead acidbattery RG-350.Note:
this STC is issued for the purpose of
transfering STC No. 10028452from Airalpha
A/S (DOA 21J.268) to new STC holder
Scandinavian AvionicsDesign GmbH (DOA
21J.014)
EASA.R.S.01449 EUROCOPTER FRANCE AS
365N
EUROCOPTER FRANCE AS
365N1
EUROCOPTER FRANCE AS
365N2
EUROCOPTER FRANCE AS
365N3
ATR 42-200/300/320 Installation of Rockwell Collins TCAS-94
System with Single TDR-94DSystem, as per
Scandinavian Avionics Engineering Order
2056096-EO issue1 dated 27th September
2010 or later EASA approved revisions.
The limitations according to Aircraft Flight
Manual Supplement2054628-AM are
applicable.
The installation of this modification by
third persons is subject towritten
permission of the approval holder and
disposal of the approvedappropriate
documentation.Prior to installation of this
modification it must be determined
thatthe interrelationship b
30.03.2012
1) Prior to installation of this modification 18.08.2009
the installer mustdetermine that the
interrelationship between this modification
and anyother previously installed
modification will introduce no adverse
effectupon the airworthiness of the
product. 2) The inst
None 1. Prior to installation of this modification 31.08.2009
the installer mustdetermine that the
interrelationship between this modification
and anyother previously installed
modification will introduce no adverse
effectupon the airworthiness of the
product.2. The insta
Limited to: S/N 650-7001 thru 650-7119 This Prior to installation of this modification it 30.11.2009
STC applies only for Single or Dual FMS GNS- must be determined thatthe
XL or GNS-XLSconfiguration, approved for B- interrelationship between this modification
RNAV operation. Intermixing with other FMSis and any other previouslyinstalled
not approved within this STC.
modification and/ or repair will introduce
no adverse effectupon the airworthiness
of the product.
- S/N 0501 and subsequent,,- Pitot heat and
Search Light must not be installed,,
Not Applicable 10.12.2009
None The approval holder shall fulfill the
obligations of Part 21,
Paragraph21A.118A.The installation of
this modification by third persons is
subject towritten permission of the
approval holder.Prior to installation of this
modification the installer must be
12.12.2012
None No additional EWIS ICAS tasks over
those already identified by theoriginal TC
Holder for the applicable aircraft models
are needed asconsequence of the
implementation of this STC.Prior to
installation of this modification it must be
determined thatthe inte
11.10.2010
25.06.2009
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