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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

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