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 />
10038758 BLR AEROSPACE, L.L.C. FAA STC SA02131SE KING AIR B200GT AND<br />
Installation of a BLR Aerospace Ultimate Approval of this change in type design applies Performance Enhancement Package 22.03.2<strong>01</strong>2<br />
B200CGT<br />
Performance Package (UPP).<br />
to the above listedaircraft models only. This requires the installation of thefollowing<br />
approval should not be extended to<br />
Supplemental Type Certificates<br />
otheraircraft of this model series unless the (STC):STC Number<br />
installer determines that therelationship ,,DescriptionSA<strong>01</strong>615SE,,BLR<br />
between this change and any other previ Aerospace Winglet Installation (STC<br />
ref<strong>EASA</strong>.IM.A.S.02051)SA3366NM,,Rais<br />
beck Ram Air Recovery System (RARS)<br />
10039059 BLR AEROSPACE, L.L.C. REV. 2 FAA STC SR<strong>01</strong>865SE 1- BELL 212<br />
2- BELL 2<strong>04</strong>B, BELL 205A1<br />
10<strong>04</strong>0783 BLR AEROSPACE, L.L.C. FAA SR00798SE / LBA RC 1163 1- 2<strong>04</strong>B, 205A-1<br />
2- 212, 412, 412EP<br />
10<strong>01</strong>7218 BOGGI S.R.L. <strong>EASA</strong>.R.S.<strong>01</strong>375 EUROCOPTER FRANCE AS<br />
365N3<br />
Installation of Dual Tailboom Strakes and Day/Night VFR only, flight into known icing<br />
FastFin.Revision 1 adds Model 2<strong>04</strong>B and conditions prohibited.<br />
changes the reference to LBA STC RC 1163to<br />
<strong>EASA</strong> STC 10<strong>04</strong>0783.Revision 2 adds<br />
additional Bell 212 and 412 FMSs.<br />
Installation of Dual Tailboom Strakes. This STC Day/Night VFR only, flight into known icing<br />
revises and supersedesLBA STC RC 1163 to conditions prohibited.<br />
add the Bell Helicopter Textron Inc. Model<br />
2<strong>04</strong>B, 412and 412EP. The AB 212 is removed<br />
as it is not included in the FAA STC.<br />
KIT MDS365-P0<strong>01</strong>-00, Additional seat fitting<br />
for Eurocopter AS365N3 Helicopter in Hems<br />
configuration.<br />
10033945 BOGGI S.R.L. AS 365 N3 Kit P/N MDS365-P002-00 ,External rear view<br />
mirror.<br />
Limited to AS 365N3 S/N 6609 and 6356,<br />
previously modified by the kit Bucher P/N ARA-<br />
AS365N2-AC50.<br />
- as defined in -Boggi s.r.l. Rotorcraft Flight<br />
Manual Supplement,Owner Manual,section 4,<br />
Edition 2,Rev. 0 dtd 12/<strong>01</strong>/2<strong>01</strong>1<br />
10035798 BOGGI S.R.L. AS365N3 Installation of Draeger TI 500 "Globetrotter" Limited to:-Incubator model Draeger TI 500<br />
incubator on AS 365N3(ref. Change 365-M003- P/N TI 500, S/N 002-Helicopter model<br />
00).<br />
AS365N3 S/N 6609 & 6356<br />
10<strong>01</strong>5497 BOMBARDIER AEROSPACE <strong>EASA</strong>.IM.A.S.<strong>01</strong>260 REV. 1 TCCA STC C-LSA05-294/D CHALLENGER CL-600-2B16 Aircraft Completion 9 Passenger Interior<br />
Configuration. (ASN 5595)<br />
10<strong>01</strong>5564 BOMBARDIER AEROSPACE <strong>EASA</strong>.IM.A.S.<strong>01</strong>463 C-LSA05-181/D, ISSUE 2 BOMBARDIER BD-100-1A10 Installation of Equipment Ladder (Aft<br />
(CHALLE<br />
Equipment Bay) in accordance with<br />
MDL3808<strong>01</strong>, rev. 1 dated 11 June 2005 and<br />
compliance report BAS683800<strong>04</strong><br />
10<strong>01</strong>5565 BOMBARDIER AEROSPACE <strong>EASA</strong>.IM.A.S.<strong>01</strong>464 C-LSA05-212/D, ISSUE 1 BOMBARDIER BD-100-1A10<br />
(CHALLE<br />
Installation of a Satellite Telephone System<br />
Interfaced to an existing Flight Telephone<br />
System in accordance with MDL<br />
BAS68<strong>01</strong>0<strong>01</strong>0 Revision A dated 30 May 2005<br />
and Compliance Report BAS68380005 dated<br />
Must be installed in conjunction with FAA 19.11.2<strong>01</strong>2<br />
STC SR00798SE (<strong>EASA</strong><br />
STC10<strong>04</strong>0783).Prior 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 wi<br />
Prior to installation of this modification it 26.07.2<strong>01</strong>2<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 />
The approval holder shall fulfil the<br />
obligations of Part 21,<br />
Paragraph21A.118A. Prior to installation<br />
of this modification it must be determined<br />
thatthe interrelationship between this<br />
modification and any other<br />
previouslyinstalled modification and/ or<br />
<strong>04</strong>.12.2007<br />
21.02.2<strong>01</strong>1<br />
repa<br />
Prior to installation of this modification it 19.07.2<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 />
Restricted to Aircraft Serial Number 5595 <strong>04</strong>.<strong>04</strong>.2006<br />
1. Limited to: S/N 20<strong>01</strong>32. This STC is<br />
approved only for the product configuration as<br />
defined in the approved design data referred to<br />
in the paragraph "Description". Compatibility<br />
with other aircraft/engine configurations shall<br />
be determined by the install<br />
1. This STC is limited to BD-100-1A10<br />
(Challenger 300) SN 20<strong>01</strong>3<br />
10<strong>01</strong>5567 BOMBARDIER AEROSPACE <strong>EASA</strong>.IM.A.S.<strong>01</strong>474 REV 1 TCCA STC C-LSA06-<strong>01</strong>5/D ISSUE 2 BOMBARDIER CL-600-2B16<br />
10/09/2005<br />
Aircraft Completion Restricted to ASN 5605 27.09.2006<br />
10<strong>01</strong>5603 BOMBARDIER AEROSPACE <strong>EASA</strong>.IM.A.S.<strong>01</strong>539 TCCA STC C-LSA05-314/D BOMBARDIER CL-600-2B16 Aircraft Completion 11 PassengerInterior 1. Restricted to Aircraft Serial Number<br />
28.11.2005<br />
Configuration<br />
5599.2. This STC is approved only for the<br />
product configuration as defined in the<br />
approved design data referred to in the<br />
paragraph "Description". Compatibility with<br />
other aircraft/engine configurations shall b<br />
10<strong>01</strong>5674 BOMBARDIER AEROSPACE <strong>EASA</strong>.IM.A.S.<strong>01</strong>654 REV 1 TCCA STC C-LSA06-025/D BOMBARDIER CL-600-2B16 Aircraft Completion, 10 Passenger Interior. 1. Restricted to ASN 5613.2. This STC is<br />
approved only for the product configuration as<br />
defined in the approved design data referred to<br />
in the paragraph "Description". Compatibility<br />
with other aircraft/engine configurations shall<br />
be determined by the insta<br />
26.10.2006<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 117/<strong>462</strong><br />
23.09.2005<br />
05.10.2005