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>7157 AEROLITE MAX BUCHER AG <strong>EASA</strong>.R.S.<strong>01</strong>265 EUROCOPTER DEUTSCHLAND APC-06-006 EMS equipment installation fro<br />
24.07.2006<br />
MBB-BK<br />
BK-117-C2 (EC145), part number 145221-5<strong>01</strong><br />
10<strong>01</strong>7164 AEROLITE MAX BUCHER AG <strong>EASA</strong>.R.S.<strong>01</strong>272 EUROCOPTER DEUTSCHLAND Installation of EMS equipment Aerolite P/N Only S/N 0<strong>04</strong>1 15.06.2006<br />
EC-135<br />
135570-5<strong>01</strong><br />
10<strong>01</strong>7172 AEROLITE MAX BUCHER AG <strong>EASA</strong>.R.S.<strong>01</strong>286 REV. 1 EUROCOPTER DEUTSCHLAND Installation of EMS Equipment P/N 135500- Prior to installation of this modification the<br />
29.05.2008<br />
EC-135-<br />
5<strong>01</strong> or P/N 135500-502. This revision extends installer must determine that the<br />
the applicability to \ec135P2+ and EC135T2+. interrelationship between this modification and<br />
any other previously installed modification will<br />
introduce no adverse effect upon the<br />
airworthiness of the product.<br />
10<strong>01</strong>7187 AEROLITE MAX BUCHER AG <strong>EASA</strong>.R.S.<strong>01</strong>324 REV. 1 EC135 P2(CPDS), P2+<br />
EMS Equipment P/N 135572-5<strong>01</strong>Change This STC is limited to aircraft with S/N 0337 The approval holder shall fulfill the 22.06.2<strong>01</strong>0<br />
EC135 T2(CPDS), T2+<br />
covered by Rev. 1 to<br />
and subsequent onlyThis STC is approved only obligations of Part 21,Paragraph<br />
<strong>EASA</strong>.R.S.<strong>01</strong>324:Installation of EMS Retainer for the product configuration as defined inthe 21.A109Prior to installation of this<br />
Set P/N 135742-5<strong>01</strong> into Aerolite<br />
approved design data referred to in the modification it must be determined<br />
EMSEquipment P/N 135572-5<strong>01</strong><br />
paragraphs "Description" and"Associated thatthe interrelationship between this<br />
Technical Documentation". Compatibilit modification and any other<br />
previouslyinstalled modification and/ or<br />
10<strong>01</strong>7194 AEROLITE MAX BUCHER AG <strong>EASA</strong>.R.S.<strong>01</strong>331 AGUSTA AB-139<br />
AGUSTA AW-139<br />
10<strong>01</strong>7209 AEROLITE MAX BUCHER AG <strong>EASA</strong>.R.S.<strong>01</strong>361 AGUSTA AB-139<br />
AGUSTA AW-139<br />
10<strong>01</strong>7214 AEROLITE MAX BUCHER AG <strong>EASA</strong>.R.S.<strong>01</strong>371 EUROCOPTER AS365 SERIES<br />
EUROCOPTER DEUTSCHLAND<br />
EC-135<br />
EUROCOPTER DEUTSCHLAND<br />
EC-135-<br />
EUROCOPTER DEUTSCHLAND<br />
10<strong>01</strong>7215 AEROLITE MAX BUCHER AG <strong>EASA</strong>.R.S.<strong>01</strong>372 EUROCOPTER DEUTSCHLAND<br />
EC-135-<br />
EUROCOPTER DEUTSCHLAND<br />
EC-635<br />
EUROCOPTER DEUTSCHLAND<br />
EC-635-<br />
10<strong>01</strong>7216 AEROLITE MAX BUCHER AG <strong>EASA</strong>.R.S.<strong>01</strong>373 EUROCOPTER DEUTSCHLAND<br />
EC-135<br />
EUROCOPTER DEUTSCHLAND<br />
EC-635<br />
10<strong>01</strong>7217 AEROLITE MAX BUCHER AG <strong>EASA</strong>.R.S.<strong>01</strong>374 REV. 1 SEE ATTACHED <strong>EASA</strong><br />
APPROVED TYP<br />
EC-635<br />
EMS Medical Rack Installation p/n 139099-5<strong>01</strong> EMS (Medevac) electrical provisions<br />
3G2564A<strong>01</strong>441 must be installed with<br />
modifications according to 3G2564W002<strong>01</strong><br />
(page 1 only).<br />
P/N 139086-5<strong>01</strong>.The equipment contains a<br />
specific cabin floor layer, 2 medical seats<br />
installed in the aft part of the cabin, one or 2<br />
stretchers, amedical supply cabinet and various<br />
stowage compartments.<br />
Armasuisse1 LH Stretcher Installation. P/N<br />
135586-5<strong>01</strong>.<br />
Armasuisse 2 RH Stretcher Installation P/N<br />
135587-5<strong>01</strong>.<br />
Life Support Module installation:P/N 135588-<br />
5<strong>01</strong>. The installation consists of a stowage<br />
provision for up to three oxygen bottles. The is<br />
module installed in the forward part of the<br />
passenger cabine.<br />
EMS Stretcher InstallationInstallation P/N<br />
135525-5<strong>01</strong>, -502 for R/H side and -503, -5<strong>04</strong><br />
for the L/H side.Note: This change to<br />
<strong>EASA</strong>.R.S.<strong>01</strong>374 introduces a new stretcher<br />
installation on the left hand side of the<br />
1. When oxygen is installed No smoking<br />
permitted.2. The occupant of the LH FWD<br />
Aft facing seat must wear a helmet.3. When<br />
the secondary stretcher is occupied the head<br />
protection pad must be installed between the<br />
stretchers.4. Following equipmen<br />
Prior to installation of this modification the<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 />
Prior to installation of this modification the<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 />
1. P/N 135525-5<strong>01</strong> and -503 are eligible for<br />
installation in S/N up to 03362. P/N 135525-<br />
502 and -5<strong>04</strong> are eligible for installation in S/N<br />
0337 and up3. Prior to installation of this<br />
modification the installer must determine that<br />
the interrelations<br />
10<strong>01</strong>7229 AEROLITE MAX BUCHER AG <strong>EASA</strong>.R.S.<strong>01</strong>400<br />
rotorcraft.<br />
EUROCOPTER DEUTSCHLAND EMS Stretcher Installation Police Thüringen<br />
12.11.2008<br />
BK117 C<br />
(Aerolite P/N 145285-5<strong>01</strong>).<br />
10<strong>01</strong>7231 AEROLITE MAX BUCHER AG <strong>EASA</strong>.R.S.<strong>01</strong>403 REV. 1 AGUSTA AB-139<br />
Installation P/N 139084-5<strong>01</strong> for 3 stretcher 1. Agusta EMS (Medevac) electrical<br />
28.11.2007<br />
AGUSTA AW-139<br />
units with relevant cabin floor rails and featuring provisions 3G2564A<strong>01</strong>411 must be installed<br />
each, dedicated oxygen and electrical with modifications according<br />
distribution systems and oxygen bottles 3G2564W002<strong>01</strong>.2. When oxygen is installed<br />
stowage provisions.<br />
No smoking permitted.3. Required minimum<br />
crew is defined in FMS-07-008.4. The<br />
dimensional limitat<br />
10<strong>01</strong>7232 AEROLITE MAX BUCHER AG <strong>EASA</strong>.R.S.<strong>01</strong>406 REV. 1 EC 135 T2, EC 135 P2,<br />
EMS Stretcher Installation P/N 135591- To ensure patient head protection from injuries Prior to installation of this modification it 20.<strong>04</strong>.2<strong>01</strong>0<br />
EC 135 T2+, EC 135 P2+ 5<strong>01</strong>.Introduction of the Cirrus Stretcher Model during crash, there mustbe at least 200mm of must be determined thatthe<br />
EC 135, EC 135 T1, EC 135 P1, CI-1 <strong>01</strong> 0-123-<strong>01</strong> into thealready certified space between the forward end of each interrelationship between this modification<br />
EC635 P2+<br />
Cirrus 1<strong>01</strong>0 Stretcher Installation P/N135574- installedstretchers and any equipment installed and any other previouslyinstalled<br />
EC635 T1 (CDPS), EC635 T2+ 5<strong>01</strong>/-502/-503/-5<strong>04</strong> (STC <strong>EASA</strong>.R.S.<strong>01</strong>406) forward of the stretchers.<br />
modification and/ or repair will introduce<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
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08.03.2007<br />
21.11.2007<br />
03.07.2007<br />
03.07.2007<br />
31.10.2007<br />
24.02.2009