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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 />

<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 27/<strong>462</strong><br />

08.03.2007<br />

21.11.2007<br />

03.07.2007<br />

03.07.2007<br />

31.10.2007<br />

24.02.2009

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