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>7099 ECMS AVIATION SYSTEMS GMBH <strong>EASA</strong>.R.S.<strong>01</strong>023 EUROCOPTER FRANCE AS 350 Installation of External Load Box ELB<strong>01</strong> This STC is approved only for the product<br />
30.<strong>01</strong>.2006<br />
B<br />
configuration as defined in the approved design<br />
EUROCOPTER FRANCE AS 350<br />
data referred to in the paragraph "Description".<br />
B1<br />
Compatibility with other aircraft/engine<br />
EUROCOPTER FRANCE AS 350<br />
configurations shall be determined by the<br />
B2<br />
EUROCOPTER FRANCE AS 350<br />
B3<br />
EUROCOPTER FRANCE AS 350<br />
BA<br />
EUROCOPTER FRANCE AS 350<br />
BB<br />
EUROCOPTER FRANCE AS 350<br />
D<br />
installer.<br />
10<strong>01</strong>7173 ECMS AVIATION SYSTEMS GMBH <strong>EASA</strong>.R.S.<strong>01</strong>288 EUROCOPTER DEUTSCHLAND Balance Weighing System BWS02. The Balnce Weighing System BWS02 is<br />
20.07.2007<br />
EC-135<br />
compatible with the following EC135 cargo<br />
hook installations:Dual External Cargo Hook<br />
(Eurocopter FMS 9.2-47) orExternal Cargo<br />
Hook (Eurocopter FMS 9.2-19).Fixed<br />
provisions including internal wiring harness are<br />
required<br />
10<strong>01</strong>7200 ECMS AVIATION SYSTEMS GMBH <strong>EASA</strong>.R.S.<strong>01</strong>349 REV. 2 EUROCOPTER DEUTSCHLAND "Load Attachment Device EAD<strong>01</strong>"Provides Prior to installation of this modification the<br />
11.12.2008<br />
EC-135-<br />
attachment provisions on rotorcraft for fast installer must determine that the<br />
EUROCOPTER DEUTSCHLAND roping / rappelling and Human External Cargo interrelationship between this modification and<br />
EC-635<br />
operations.Revision 1 to the STC is a revision any other previously installed modification will<br />
EUROCOPTER DEUTSCHLAND of the previous LBA STC No. 1025, dated introduce no adverse effect upon the<br />
EC-635-<br />
24.11.2003. Revision 1 adds applicable m airworthiness of the product. The install<br />
10<strong>01</strong>72<strong>01</strong> ECMS AVIATION SYSTEMS GMBH <strong>EASA</strong>.R.S.<strong>01</strong>350 REV. 1 <strong>EASA</strong> STC 1025 EUROCOPTER DEUTSCHLAND<br />
BK117 C<br />
10<strong>01</strong>7250 ECMS AVIATION SYSTEMS GMBH <strong>EASA</strong>.R.S.<strong>01</strong>451 EUROCOPTER FRANCE AS<br />
365N3<br />
EUROCOPTER FRANCE EC 155<br />
B1<br />
EUROCOPTER FRANCE EC<br />
155B<br />
EUROCOPTER FRANCE SA<br />
10<strong>01</strong>7273 ECMS AVIATION SYSTEMS GMBH <strong>EASA</strong>.R.S.<strong>01</strong>503 EUROCOPTER DEUTSCHLAND<br />
EC-135-<br />
EUROCOPTER DEUTSCHLAND<br />
EC-635<br />
EUROCOPTER DEUTSCHLAND<br />
EC-635-<br />
365C2<br />
“External Abseil Device EAD<strong>01</strong>”Provides<br />
attachment provisions on rotorcraft for fast<br />
roping / rappelling and Human External Cargo<br />
operations.This STC is a revision of the<br />
previous <strong>EASA</strong> STC No. 1025, dated<br />
24.11.2003The Technical Changes are as<br />
follows:-<br />
1. The scope of this STC is limited to<br />
attachment provisions for rappelling / fast<br />
roping and HEC operations. It does not include<br />
all the necessary equipment like ropes and<br />
personal carrying device. It does not establish<br />
all the procedures necessary for<br />
External Load Attachment Device EDX02. The scope of this STC is limited to technical<br />
provisions to the helicopter. It does not include<br />
ropes and personal equipment, training<br />
aspects and operation procedures necessary<br />
for the fast roping operation. These procedures<br />
must be established by the ope<br />
Installation of HEC Rope System HRS<strong>01</strong>, P/N<br />
HRS<strong>01</strong>-<strong>01</strong>-00.00<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 />
10<strong>01</strong>7282 ECMS AVIATION SYSTEMS GMBH <strong>EASA</strong>.R.S.<strong>01</strong>530 EUROCOPTER DEUTSCHLAND Installation of HEC Rope System HRS<strong>01</strong>, P/N<br />
MBB-BK<br />
HRS<strong>01</strong>-<strong>01</strong>-00.00<br />
10<strong>01</strong>7283 ECMS AVIATION SYSTEMS GMBH <strong>EASA</strong>.R.S.<strong>01</strong>531 EUROCOPTER FRANCE AS 350 External Antenna for Transceiver System 1. This STC provides approval for structural<br />
B1<br />
ATS<strong>01</strong> installation on the ldg gear crosstube. and electrical provisions only. Installation and<br />
EUROCOPTER FRANCE AS 350<br />
operation of any equipment to be connected to<br />
B2<br />
the external antenna shall be covered by<br />
EUROCOPTER FRANCE AS 350<br />
separate approval.2. Prior to installation of<br />
B3<br />
EUROCOPTER FRANCE AS 350<br />
BA<br />
EUROCOPTER FRANCE AS 350<br />
BB<br />
EUROCOPTER FRANCE AS 350<br />
D<br />
EUROCOPTER FRANCE AS<br />
350B<br />
this modification the i<br />
10<strong>01</strong>7293 ECMS AVIATION SYSTEMS GMBH <strong>EASA</strong>.R.S.<strong>01</strong>566 BELL 206A<br />
Installation of Bifilar Cargo System 1) Prior to installation of this modification the<br />
BELL 206A-1<br />
installer must determine that the<br />
BELL 206B<br />
interrelationship between this modification<br />
BELL 206B-1<br />
andany other previously installed modification<br />
BELL 206L<br />
will introduce no adverse effect upon the<br />
BELL 206L-1<br />
BELL 206L-3<br />
BELL 206L-4<br />
airworthiness of the product.2) The ins<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 197/<strong>462</strong><br />
30.<strong>01</strong>.2007<br />
18.07.2008<br />
11.12.2008<br />
19.12.2008<br />
03.03.2009<br />
08.06.2009
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