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 />
10030099 AVIONICS INTEGRATION &<br />
MBB-BK 117 C-1 Cabin Interior RetrofitInstallation of a cabin S/N 7541 Prior to installation of this modification it 21.05.2<strong>01</strong>0<br />
ENGINEERING<br />
interior retrofit based on AIEC engineeringorder<br />
must be determined thatthe<br />
854-062.<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 />
10030961 AVIONICS INTEGRATION &<br />
ENGINEERING<br />
10032056 AVIONICS INTEGRATION &<br />
ENGINEERING<br />
10033418 AVIONICS INTEGRATION &<br />
ENGINEERING<br />
10035543 AVIONICS INTEGRATION &<br />
ENGINEERING<br />
10037002 AVIONICS INTEGRATION &<br />
ENGINEERING<br />
10038857 AVIONICS INTEGRATION &<br />
ENGINEERING<br />
10038859 AVIONICS INTEGRATION &<br />
ENGINEERING<br />
10038860 AVIONICS INTEGRATION &<br />
ENGINEERING<br />
10039495 AVIONICS INTEGRATION &<br />
ENGINEERING<br />
BEECH 200 Installation of HySpex Camera System (NEO) Only aeroplanes in compliance with the<br />
preconditions as listed inChapter C of<br />
Engineering Order, Doc. No. CV877-062,<br />
Revision A, dated14-Jul-2<strong>01</strong>0, or later<br />
approved revision, are eligible for this change.<br />
35A / 36A COMJAM System Installation This COMJAM system installation approval is<br />
only applicable to thefollowing aircraft<br />
equipped with certain special mission<br />
provisions(including electrical power supply,<br />
harnesses and wiring, workstationand<br />
antennas): s/n's 35A-139, 35A-179, 35A-268,<br />
35A-33<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<br />
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 />
P-<strong>EASA</strong>.A.S.03870 PA-31T TAS 620 System Installation by installing an<br />
Avidyne TAS 620 TrafficAdvisory System<br />
None None 03.07.2009<br />
EC135 P2+ GNS-530 & GNS-430A InstallationOut: Garmin This <strong>EASA</strong> STC is only valid after <strong>EASA</strong> The approval holder shall fulfil the 29.06.2<strong>01</strong>1<br />
GNS-530W & GNS-430WIn: Garmin GNS-530 Validation of FAA STC SR09137RC- obligations of Part 21,<br />
& GNS-430AComplete retrofit done by D(Extended R/H Side Instrument Panel).S/N: Paragraph21.A109. Prior to installation of<br />
American Eurocopter under FAA Form 337 0684<br />
this modification it must be determined<br />
dated11.12.2009 and FAA Form 8110-3 dated<br />
thatthe interrelationship between this<br />
11.12.2009<br />
modification and any other<br />
previouslyinstalled modification and/ or<br />
repai<br />
HAWKER 900XP Cabin Interior Removal and Modification. None. None. 24.10.2<strong>01</strong>1<br />
16.07.2<strong>01</strong>0<br />
05.10.2<strong>01</strong>0<br />
CL-600-2B16 Iridium Satcom Installation (ICG) None The e-phone, base station and docking<br />
station units not installed, thesame will be<br />
performed under DOA minor change<br />
separately.Prior to installation of this<br />
modification it must be determined<br />
thatthe interrelationship between this<br />
modification and any othe<br />
20.03.2<strong>01</strong>2<br />
CL-600-2B16 Terrain Awareness and Warning System<br />
(TAWS) Upgrade to SCN 12.0 (UASC)<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 />
20.03.2<strong>01</strong>2<br />
CL-600-2B16 CVR-120 replacement by CVR-120R (UASC) 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 />
20.03.2<strong>01</strong>2<br />
REV. 1 35A/36A Enhanced Surveillance Upgrade to MST 67A<br />
Transponder (Honeywell)<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 />
16.05.2<strong>01</strong>2<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 99/<strong>462</strong>
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