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 />
10039579 NEW SYSTEMS ENGINEERING REV. 1 FAA STC ST10977SC DHC-8-102/-103/-106<br />
Installation of Dual Universal Avionics Flight Installation is limited to serial numbers listed in Prior to installation of this modification it 21.05.2<strong>01</strong>2<br />
DHC-8-2<strong>01</strong>/-202<br />
Management Systems (FMS)with Global the latest approvedversion of FMS Instruction must be determined thatthe<br />
DHC-8-3<strong>01</strong>/-311/-314/-315 Positioning System (GPS)FAA STC<br />
Top Drawing 379-02-00<strong>01</strong>.<br />
interrelationship between this modification<br />
ST10977SC<br />
and any other previouslyinstalled<br />
modification and/ or repair will introduce<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
10<strong>04</strong>0905 NEXTANT AEROSPACE L.L.C. FAA STC ST03960AT 400A Installation of Rockwell Collins Venue In-Flight<br />
Entertainment (IFE),Aircell Axxess Cabin II<br />
Iridium Phone and High Speed Internet<br />
Systemwith Wireless Local Area Network<br />
(WLAN) Astronics 115V AC 60 Hz<br />
CabinInverter, and Emteq LED Cabin Lighting<br />
System.<br />
10<strong>04</strong>0906 NEXTANT AEROSPACE L.L.C. FAA STC ST03110CH 400A Installation of L3 Communications Digital Flight<br />
Data Recorder.<br />
10<strong>04</strong>2091 NEXTANT AEROSPACE L.L.C. FAA STC ST10959SC BEECHJET 400A Installation of Rockwell Collins Pro Line 21<br />
Electronic FlightInstrument System (EFIS) with<br />
Rockwell Collins FMS-6100,<br />
Localiserperformance with Vertical Guidance<br />
(LPV) approach capability andUniversal<br />
Systems Company (UASC) Terrain awareness<br />
warning Syste<br />
10<strong>04</strong>2353 NEXTANT AEROSPACE L.L.C. FAA STC ST02371LA 400A Installation of Williams International FJ44-3AP<br />
engines as replacementfor the original Pratt &<br />
Whitney Canada JT15D-5 units.<br />
10<strong>04</strong>0787 NORTH FLIGHT DATA SYSTEMS, L.L.C. FAA STC SR09468RC EC135 P1, EC135 P2,<br />
EC135 P2+, EC135 T1,<br />
EC135 T2, EC135 T2+<br />
10<strong>01</strong>6294 NORTHEAST ENGINEERING &<br />
DEVELOPMENT<br />
10<strong>01</strong>7039 NORTHEAST ENGINEERING &<br />
DEVELOPMENT<br />
This STC is intended to provide internet<br />
connection and E-Mail servicesto the aircraft<br />
cabin using portable electronic devices<br />
(PED's). Anyother intended function of this<br />
equipment will require a re-examinationof the<br />
certification basis.<br />
Prior to installation of this modification it 02.08.2<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 />
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 />
02.08.2<strong>01</strong>2<br />
None. For aircraft equipped with Williams FJ44- 07.11.2<strong>01</strong>2<br />
3AP Engines, those engines mustbe<br />
installed under FAA STA ST02371LA.<br />
Aircraft must have previously qualified for<br />
Operations in ReducedVertical Airspace<br />
via: - RK-1 through RK-117 and RK-119<br />
through RK-139, Hawker B<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 />
26.11.2<strong>01</strong>2<br />
Installation of the Outerlink Corporation CP-3 or none Use of Electronic Flight Bag (EFB) with<br />
CP-3i Automatic FlightFollowing System,<br />
optional N0<strong>04</strong>-4000 OCP shall bein<br />
Optional Electronic Flight Bag Provisions, and<br />
accordance with Advisory Circular AC<br />
FlightData System in accordance with North<br />
120-76A and may requireoperational<br />
Flight Data System, LLC MasterInstallation List,<br />
approval.Prior to installation of this<br />
Document N° NL<strong>462</strong>073006, Re<br />
modification it must be determined<br />
thatthe interrelationship between th<br />
<strong>EASA</strong>.IM.A.S.02591 TCCA LSTC NO. O-LSA05-321/D IS PILATUS PC-12/45 Installation of GNS 430 (COMM/NAV/GPS), This STC is limited to Pilatus PC-12/45, Serial<br />
GNS 530 (COM/NAV/GPS), KDR 510 (Data number 659Prior to the installation of this<br />
link Weather Receiver), KGS SS50 (Static modification the installer must determine that<br />
Inverter), XMRadio Receiver with XM Radio the interrelationship between this modification<br />
Display & Control Head (Cabin), and necessary and any over previously installed modifications<br />
antennas.<br />
will introduce no adv<br />
<strong>EASA</strong>.IM.R.S.<strong>01</strong>463 TCCA STC SH97-59 ROBINSON R44<br />
Bear Paw Installation. Prior to installation of this modification the<br />
ROBINSON R44 II<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. The install<br />
10<strong>01</strong>4817 NORTHERN AVIONICS S.R.L. <strong>EASA</strong>.A.S.03025 PIPER PA-31T Installation of Mode S Diversity XPDR<br />
Honeywell MST-67A (Elementary<br />
Surveillance).<br />
10<strong>01</strong>7108 NORTHERN AVIONICS S.R.L. <strong>EASA</strong>.R.S.<strong>01</strong>084 AGUSTA A-109 A<br />
AGUSTA A-109 AII<br />
AGUSTA A-109 C<br />
NAV 277 "Installation of an alternate static<br />
system on board to rotorcraft A 109 A/AII/C"<br />
10<strong>01</strong>7115 NORTHERN AVIONICS S.R.L. <strong>EASA</strong>.R.S.<strong>01</strong>097 AGUSTA AB-412EP Installation of an EGPWS Honeywell MK XXI. 1. This STC is approved only for the product<br />
configuration as defined in the approved design<br />
data referred to in the paragraph "Description".<br />
Compatibility with other aircraft/engine<br />
configurations shall be determined by the<br />
installer.<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 344/<strong>462</strong><br />
26.07.2<strong>01</strong>2<br />
16.10.2007<br />
18.07.2008<br />
13.07.2007<br />
19.<strong>01</strong>.2006<br />
08.08.2005
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