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>04</strong>1273 BRITISH AIRWAYS PLC 747-400 B747-400 TCAS change 7.1 update 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 />
03.09.2<strong>01</strong>2<br />
10<strong>01</strong>6535 BRUCE AEROSPACE Inc. <strong>EASA</strong>.IM.A.S.02912 REV. 1 FAA STC ST00941LA BD-700-1A10 Installation of Floor Proximity Emergency<br />
Escape Path Marking System.<br />
10035636 BRUCE AEROSPACE Inc. 2003-1912 FAA STC SA6<strong>01</strong>1NM CL-600-2B16 Installation of Floor Proximity Emergency<br />
Escape Path Marking System<br />
Seat Mounted Proximity Lighting System:-Exit<br />
identifiers and flood lights (e.g. part number<br />
BR9279-series): aminimum of two out of five<br />
lamps in each part must be operative.-All light<br />
modules (e.g. part number BR9644-series): a<br />
minimum of oneout of two lam<br />
This system has been determined to comply<br />
with the applicableairworthiness requirements<br />
with the following operative lightassemblies: -<br />
Floor Mounted Proximity Lighting SystemExit<br />
identifiers and/or flood lights - 2 bulbs<br />
operative, light trackred modules<br />
10<strong>01</strong>5035 BUCHER LEICHTBAU AG <strong>EASA</strong>.A.S.03348 MD-11 Modification of New Generation Stretcher This approval is only valid for the modified<br />
(NGS) pn. 1120000-2<strong>01</strong> for installation in a MD- installation in the MD-11 on the right hand side<br />
11 on the right hand side of the fuselage, in of the fuselage.All other installations of the<br />
accordance with Bucher General Arrangement New Generation Stretcher are covered by<br />
Drawing 1120000-2<strong>01</strong>.<br />
FOCA STC No. Z25-20-60It is the<br />
responsibility of the installer to make sur<br />
10<strong>01</strong>5074 BUCHER LEICHTBAU AG <strong>EASA</strong>.A.S.034<strong>04</strong> FOCA STC: Z 25-20-53 PILATUS PC-12<br />
PILATUS PC-12/45<br />
PILATUS PC-12/47<br />
EMS installation P/N 1270<strong>01</strong>-300This <strong>EASA</strong><br />
STC extens the validity of FOCA STC Z25-<br />
2053 for PC-12 S/N up to 888.<br />
Prior to installation of this modification it 30.06.2<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.<br />
Prior to installation of this modification it 06.07.2<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.<br />
06.11.2007<br />
S/N 861-888 19.12.2007<br />
10<strong>01</strong>5092 BUCHER LEICHTBAU AG <strong>EASA</strong>.A.S.03429 PILATUS PC-12 Heavy Duty Floor Panel 19.05.2008<br />
10<strong>01</strong>5227 BUCHER LEICHTBAU AG <strong>EASA</strong>.A.S.03644 REV. 3 PILATUS PC-12/47E Bucher EMS Equipment PC-12/47E.P/N Applicable to PC12/47E series only.Smoking is The approval holder shall fulfil the 07.07.2<strong>01</strong>0<br />
<strong>01</strong>270<strong>01</strong>-400: Addition of equipment<br />
not permitted in the aircraft cabin when the obligations of Part 21,<br />
configuration P/N <strong>01</strong>270<strong>01</strong>-450<br />
oxygen bottle isinstalled.<br />
Paragraph21.A109. Prior to installation of<br />
this modification it must be determined<br />
thatthe interrelationship between this<br />
modification and any other<br />
previouslyinstalled modification and/ or<br />
repai<br />
10<strong>01</strong>6797 BUCHER LEICHTBAU AG <strong>EASA</strong>.IM.R.S.<strong>01</strong>150 EUROCOPTER DEUTSCHLAND Ambulance Rescue SystemThe FOCA STC Z This STC is approved only for the product<br />
11.11.2005<br />
BO-105<br />
25-20-49 (ambulance rescue system) was configuration as defined in the approved design<br />
validated by the LBA under the number data referred to in the paragraph "Description".<br />
0589/3025 dated 24 February 1995, approving Compatibility with other aircraft/engine<br />
installation onto the BO105SThis STC is re- configurations shall be determined by the<br />
issued as <strong>EASA</strong> STC to extend applicability to installer.<br />
BO105LS.<br />
10<strong>01</strong>7089 BUCHER LEICHTBAU AG <strong>EASA</strong>.R.S.00697 REV. 2 EUROCOPTER DEUTSCHLAND Ambulance and rescue equipment P/N ARA- 1. No smoking is allowed in the rotorcraft<br />
12.<strong>01</strong>.2007<br />
EC-135-<br />
EC135-AC65 in accordance with master cabin.2. This STC is approved only for the<br />
document list MDOC-AC65 rev D or later product configuration as defined in the<br />
approved revision. Revision 1: Change of approved design data referred to in the<br />
Converter from ARA-EC135-AC65.Revision 2: paragraphs "Description" and “Associated<br />
Inclusion of models P2+ and T2+<br />
Technical Documentation”. Compatibility wit<br />
10<strong>01</strong>7192 BUCHER LEICHTBAU AG <strong>EASA</strong>.R.S.<strong>01</strong>329 REV. 1 EC135 P1, T1, P2, T2, P2+, T2+ EMS-Equipment ARA-EC135-AC66Minor<br />
change to STC <strong>EASA</strong>.R.S.<strong>01</strong>329 to<br />
incorporate:- new mattress for the stretcher-<br />
dead end stop for the stretcher installation-<br />
additionnal stud to the center cabinet- medical<br />
equipment retainers.<br />
10<strong>01</strong>7211 BUCHER LEICHTBAU AG <strong>EASA</strong>.R.S.<strong>01</strong>367 EUROCOPTER DEUTSCHLAND<br />
EC-135-<br />
EMS Instalaltion ARA-EC135-AC61This<br />
change introduces the following new items not<br />
included in FOCA STC FOCA 25-20-<br />
108:alternative side cabinet LH (p/n<br />
1359270)new center cabinet (p/n<br />
13597<strong>01</strong>)alternative seat installation (p/n<br />
1353<strong>04</strong>0).<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. The in<br />
24.07.2009<br />
Smoking is not permitted in the rotorcraft<br />
cabin.<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 145/<strong>462</strong><br />
29.05.2007
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