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>7240 BUCHER LEICHTBAU AG <strong>EASA</strong>.R.S.<strong>01</strong>428 FOCA STC 25-20-62 EUROCOPTER DEUTSCHLAND 1. Installation of ambulance and rescue<br />
22.11.2007<br />
EC-135-<br />
equipment.2. Extension of Validity of former<br />
FOCA STC Z - 25-2062 to the new model<br />
versions T2+/P2+ of EC 135.<br />
10<strong>01</strong>7275 BUCHER LEICHTBAU AG <strong>EASA</strong>.R.S.<strong>01</strong>509 FOCA STC 25-20-64 EC-135-P1, EC-135-P2,<br />
Installation of VIP-EC135-AC63 Bucher VIP Not applicable The approval holder shall fulfil the 14.11.2008<br />
EC-135-P2+, EC-135-T1 Equipment(Revision of FOCA STC FOCA Z 25-<br />
obligations of Part 21,<br />
EC-135-T2, EC-135-T2+<br />
20-64 Issue 3)<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 />
10027691 BUCHER LEICHTBAU AG FOCA 25-20-102 REV. 4 SEE AIRCRAFT ALLOCATION 16G New Generation Stretcher P/N 1120030 S/N: as per Aircraft Allocation Table E<strong>04</strong>3-<strong>01</strong>- This STC revision replaces <strong>EASA</strong> STC 21.08.2<strong>01</strong>2<br />
REV 3<br />
TABLE<br />
SeriesMinor change to <strong>EASA</strong> STC 10027691- 12 Rev. E of 31/07/2<strong>01</strong>2This installation 10027691 Rev. 3Prior to installation of<br />
E<strong>04</strong>3-<strong>01</strong>-12 REV. E OF 31/07/12 Stretcher integration P/N 1120030-Series on constitutes an approval for installation only this modification it must be determined<br />
Airbus A321-211<br />
foraircraft serial numbers as stated in the thatthe interrelationship between this<br />
Master Document List. For anyadditional modification and any other<br />
configurations as per Aircraft Allocati previouslyinstalled modification and/ or<br />
repair will introduce no adverse<br />
10027884 BUCHER LEICHTBAU AG P-<strong>EASA</strong>.A.S.03796 REV. 2 SEE <strong>EASA</strong> APPROVED AML P/N 1120030-300 - 16g New Generation This STC does not constitute an approval for Prior to installation of this modification it <strong>01</strong>.07.2<strong>01</strong>0<br />
Stretcher XLRevision of the <strong>EASA</strong> STC installation. Compliancewith following must be determined thatthe<br />
10027884 to include A380 a/c type in requirements below need to be demonstrated interrelationship between this modification<br />
theapplicability<br />
through adesign approval for Stretcher and any other previouslyinstalled<br />
installation in aircraft per approvedModel list: § modification and/or repair will introduce<br />
25.561(d) § 25.785(a) § 25.785(h) § 25. no adverse effectupon the airworthiness<br />
of the product.<br />
10029211 BUCHER LEICHTBAU AG REV. 5 EC135 ARA-EC135-AC67 BUCHER Ambulance and<br />
Rescue System (ARA):Rev. 5 to <strong>EASA</strong> STC<br />
10029211: - Installation of a hot compartment<br />
10030689 BUCHER LEICHTBAU AG P-<strong>EASA</strong>.A.S.03797 SEE <strong>EASA</strong> APPROVED MODEL<br />
LIST<br />
intocenter cabinet Record of revisions: Rev 4: -<br />
editorial change to <strong>EASA</strong> approval certificate<br />
(correction by <strong>EASA</strong>)Rev 3: (Minor Chang<br />
16g New Generation Stretcher P/N 1120020-<br />
300 - (NGS)<br />
10030758 BUCHER LEICHTBAU AG P-<strong>EASA</strong>.A.S.03712 ERJ-170() E006-14-08 - P/N 1120050 9G NGS XL<br />
Stretcher: Installation of aremovable 9g New<br />
Generation Stretcher (NGS)<br />
10030810 BUCHER LEICHTBAU AG FOCA Z25-20-57 REV. 1 EC135 P1(CDS), EC135<br />
P1(CPDS)<br />
EC135 P2(CPDS), EC135 P2+<br />
EC135 T1, EC135 T2, EC135 T2+<br />
10031757 BUCHER LEICHTBAU AG P-<strong>EASA</strong>.A.S.03984 REV. 6 SEE AIRCRAFT ALLOCATION<br />
TABLE E-<strong>04</strong>3-02-12 REV. A<br />
DATED 10/12/2<strong>01</strong>2<br />
10038839 BUCHER LEICHTBAU AG <strong>EASA</strong>.A.S.03919 REV. 1 SEE <strong>EASA</strong> APPROVED MODEL<br />
LIST<br />
Installation of ARA-EC135-AC60 Ambulance<br />
and Rescue SystemNew revision covers:STC<br />
issuance under <strong>EASA</strong> format at revision 0,<br />
Exchange of Suction Unitwith new P/N<br />
1355185,adding P2+ and T2+ at the list<br />
of EC135 models. This STC revokes the STC<br />
1003<strong>04</strong>89<br />
ATS 16g Stretcher P/N: 1123000-000 / -100 / -<br />
200 / -300 / -390 / -400 /-500 / -590Major<br />
Change to STC 10031757 Rev. 4-Installation<br />
envelope expansion for Boeing B787-<br />
Reduction of installation limitations-Introduction<br />
of the Aircraft Allocation Table<br />
Small person restraint system P/N 1120<strong>04</strong>0 for<br />
use on 16G New GenerationStretcher P/N<br />
1120020-XXX.<br />
Compliance with NVIS compatible flight decks Prior to installation of this modification it 21.05.2<strong>01</strong>2<br />
must be demonstrated by theinstaller when must be determined thatthe<br />
ARA-EC135-AC67 with NVIS compatible cabin interrelationship between this modification<br />
lighting shallbe installed into NVIS equipped and any other previouslyinstalled<br />
rotorcraft.<br />
modification and/ or repair will introduce<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
This STC does not constitute an approval for Prior to installation of this modification it <strong>01</strong>.07.2<strong>01</strong>0<br />
installation. Compliancewith following must be determined thatthe<br />
requirements below need to be demonstrated interrelationship between this modification<br />
through adesign approval for Stretcher and any other previouslyinstalled<br />
installation in aircraft per approvedModel list: § modification and/ or repair will introduce<br />
25.561(d) § 25.785(a) § 25.785(h) § 25. no adverse effectupon the airworthiness<br />
of the product.<br />
-Limitations iaw. User Manual E<strong>01</strong>7-<strong>01</strong>-08-<br />
TGM 25/12 addressed per CRI D-1 A.S.3712<br />
None. 13.07.2009<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 />
29.11.2<strong>01</strong>1<br />
This STC constitutes an approval for<br />
installation only for aircraftserial numbers as<br />
stated in the Master Document List. For any<br />
additionalconfiguration as per Aircraft<br />
Allocation Table, the requirements asstated in<br />
the Master Document List have to be demo<br />
Small person restraint to be used only on<br />
stretcher P/N 1120020-XXX.Occupant<br />
limitations as per General Arrangement<br />
drawing 1120<strong>04</strong>0 and UserManual E<strong>01</strong>7-<strong>04</strong>-<br />
08.<br />
This <strong>EASA</strong> STC amends STC 10031757<br />
Rev. 5Prior to installation of this<br />
modification it must be determined<br />
thatthe interrelationship between this<br />
modification and any other<br />
previouslyinstalled modification and/ or<br />
repair will introduce no adverse<br />
14.12.2<strong>01</strong>2<br />
effectupon<br />
The installation of this modification by 20.03.2<strong>01</strong>2<br />
third persons is subject towritten<br />
permission of the approval holder and<br />
holding and disposal ofthe approved<br />
appropriate documentation.Prior to<br />
installation of this modification it must be<br />
determined thatthe interre<br />
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