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 />
10<strong>01</strong>7087 AIR AMBULANCE TECHNOLOGY <strong>EASA</strong>.R.S.0<strong>04</strong>62 REV. 3 EC 135 Installation of Air Ambulance Equipment, 1. Subject to compliance with the provisions<br />
08.10.2008<br />
GES.m.b.H.<br />
Mission Equipment, Airborne Radiation of EC 1702/2003 PART 21 Subpart E, this<br />
Measuring Equipment, Revision2 addsVIP Certificate and associated data shall remain<br />
Interior P/N 135-25-20-5000-900 incl. flooring, valid until surrendered, withdrawn or other<br />
seats, fairing and cabinets.<br />
terminated.2. This STC is approved only for<br />
the product configuration as d<br />
10<strong>01</strong>7112 AIR AMBULANCE TECHNOLOGY<br />
GES.m.b.H.<br />
10<strong>01</strong>7225 AIR AMBULANCE TECHNOLOGY<br />
GES.m.b.H.<br />
10<strong>01</strong>7254 AIR AMBULANCE TECHNOLOGY<br />
GES.m.b.H.<br />
10<strong>01</strong>7291 AIR AMBULANCE TECHNOLOGY<br />
GES.m.b.H.<br />
10031521 AIR AMBULANCE TECHNOLOGY<br />
GES.m.b.H.<br />
10032292 AIR AMBULANCE TECHNOLOGY<br />
GES.m.b.H.<br />
10034706 AIR AMBULANCE TECHNOLOGY<br />
GES.m.b.H.<br />
100372<strong>01</strong> AIR AMBULANCE TECHNOLOGY<br />
GES.m.b.H.<br />
10037231 AIR AMBULANCE TECHNOLOGY<br />
GES.m.b.H.<br />
10038064 AIR AMBULANCE TECHNOLOGY<br />
GES.m.b.H.<br />
<strong>EASA</strong>.R.S.<strong>01</strong>089 BELL 407 Mission Equipment Bell 407 – Several racks to<br />
install a camera equipment for TV productions<br />
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 />
<strong>EASA</strong>.R.S.<strong>01</strong>393 AS 332 L2 VIP interior, quick conversion P/N 332-25-24installer.<br />
1. STC applicable only on individual<br />
3000-9<strong>01</strong>.<br />
AS332L2 aircraft equipped with approved VIP<br />
salon consisting of Eurocopter<br />
furniture:Forward Lounge: 4 face-to-face VIP<br />
seats with 2 VIP tables in the middle based on<br />
Eurocopter Dwg 332V851329.Rear Lounge: 8<br />
comfort<br />
<strong>EASA</strong>.R.S.<strong>01</strong>457 W-3AS Installation of Air Ambulance Equipment "quick<br />
conversion P/N W-3A-25-20-33.000.<br />
<strong>EASA</strong>.R.S.<strong>01</strong>548 AB 139, AW 139 Installation of Air Ambulance Equipment, 1) Prior to installation of this modification the<br />
Mission Equipment "Quick - Conversion", P/N installer must determine that the<br />
AW139-25-20-37.000-60x model<br />
interrelationship between this modification<br />
andany other previously installed modification<br />
will introduce no adverse effect upon the<br />
airworthiness of the product.2) The ins<br />
REV. 1 ASTRA SPX Installation of Air Ambulance Equipment In<br />
Astra SPX<br />
A330-200/ -300 Air Ambulance Equipment "quick<br />
conversion"P/N A330-25-20-10.000 515 -<br />
Intensive Care Module P/NA330-25-20-10.300-<br />
603<br />
<strong>EASA</strong>.R.S.0<strong>04</strong>70 REV.1 AS 350 B, AS 350 B1, AS 350 B2 Installation of Air Ambulance Equipment<br />
AS 350 B3, AS 350 BA,EC 130 B4 (removable stretcher)<br />
<strong>EASA</strong>.R.S.0<strong>04</strong>64 REV. 3 1. BHT 212/412/412 EP<br />
2. AB 212/AB 412/412 EP<br />
Installation of Air Ambulance<br />
EquipmentExtension of existing<br />
<strong>EASA</strong>.R.S.0<strong>04</strong>64 Rev. 2 with Helicopter Model<br />
412EP<br />
02.11.2005<br />
17.08.2007<br />
17.<strong>04</strong>.2008<br />
09.06.2009<br />
For S/N 133: Limited to Astra SPX, S/N 133 Prior to installation of this modification it 13.02.2<strong>01</strong>2<br />
with Duncan Interior STC ST00808 WIinstalled. must be determined thatthe<br />
and modified according this <strong>EASA</strong> STCThis interrelationship between this modification<br />
STC requires implementation of Two (2) Minor and any other previouslyinstalled<br />
changes:Avionics Integration & Engineering modification and/ or repair will introduce<br />
Corporation AG, CH : Removal ofpart no adverse effectupon the airworthiness<br />
of the product.<br />
This STC does not constitute an approval for<br />
installation. Compliancewith the following<br />
requirements will be demonstrated and<br />
covered by theDOA responsible for the<br />
medical stretcher installation on the<br />
aircraftA330 through a design approval: §<br />
25.561(d) §<br />
Prior to installation of this modification it 25.10.2<strong>01</strong>0<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 none 20.<strong>04</strong>.2<strong>01</strong>1<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 />
11.11.2<strong>01</strong>1<br />
MYSTERE FALCON 50 Installation of Air Ambulance Equipment "quick None. Prior to installation of this modification it 11.11.2<strong>01</strong>1<br />
conversion" in MF50 inthe RH Cabin Section of<br />
must be determined thatthe<br />
Aircraft.<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 />
LEARJET 45 Installation of Air Ambulance Equipment Minor Change LR45-19<strong>01</strong>0-050-LP, Installation Prior to installation of this modification it 16.<strong>01</strong>.2<strong>01</strong>2<br />
of EMS power source must beinstalled prior must be determined thatthe<br />
this modification<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> 49/<strong>462</strong>
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