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>04</strong>1125 BELL HELICOPTER TEXTRON, Inc. FAA SR00741DE BELL 429 Removable Crew Door Installation Kit (P/N 429- None If the holder agrees to permit another 22.08.2<strong>01</strong>2<br />
650-0<strong>01</strong>/3/4) for BellHelicopter Textron Model<br />
person to use this certificate toalter the<br />
429 Helicopters.<br />
product, the holder shall give the other<br />
person writtenevidence of that<br />
permission.Prior to installation of this<br />
modification it must be determined<br />
thatthe interrelationship<br />
10<strong>04</strong>1215 BELL HELICOPTER TEXTRON, Inc. FAA STC SR09541RC 407 Passenger Sliding Doors Kit P/N 407-270-003 1. The Passenger Sliding Doors Kit P/N 407- If the holder agrees to permit another 30.08.2<strong>01</strong>2<br />
for Bell Helicopter TextronModel 407<br />
270-003 modifies the hingedpassenger doors person to use this certificate toalter the<br />
Helicopters.Reference FAA STC SR0941RC. for the Bell Helicopter Textron Canada Limited product, the holder shall give the other<br />
(BHTCL)Model 407 Helicopters. A Personnel person writtenevidence of that<br />
attachment Fixture mounted in thepassenger permission.Prior to installation of this<br />
compartment is not intended to secure modification it must be determined<br />
thatthe interrelationship<br />
10<strong>04</strong>1217 BELL HELICOPTER TEXTRON, Inc. FAA STC SR09540RC 407 Crew Area Hardpoints Kit BHTI P/N 407-240- 1. High skid landing gear is required for BHTI - The Kits approved in this STC can be 30.08.2<strong>01</strong>2<br />
0<strong>01</strong>Internal Hardpoint Kit BHTI P/N 407-638- P/N 407-638-0<strong>01</strong> ExternalHardpoint Kit installed individually or in anycombination-<br />
0<strong>01</strong>External Hardpoint Kit BHTI P/N 407-230- installation.2. Installation of BHTI P/N 407-270- If the holder agrees to permit another<br />
0<strong>01</strong> and P/N 407-230-100Pylon Hardpoint Kit 003 Passenger Sliding Doors Kit(separate person to use this certificateto alter the<br />
BHTI P/N 407-854-0<strong>01</strong>/2/3Reference FAA STC) is a co-requisite for BHTI P/N 407-854- product, the holder shall give the other<br />
STC SR09540RC<br />
0<strong>01</strong>/2/3 PylonHardpoints Kit installat<br />
person writtenevidence of that<br />
permission.Prior t<br />
10<strong>04</strong>1283 BELL HELICOPTER TEXTRON, Inc. FAA STC SR02405LA 407 Survivor Window Raft Kit P/N 407-567-002 for None If the holder agrees to permit another<br />
Bell Helicopter TextronModel 407<br />
person to use this certificate toalter the<br />
Helicopters.Reference FAA STC SR02405LA.<br />
product, the holder shall give the other<br />
person writtenevidence of that<br />
permission. Prior to installation of this<br />
modification it must be determined<br />
thatthe interrelationship<br />
10<strong>01</strong>5578 BENZ AIRBORNE SYSTEMS <strong>EASA</strong>.IM.A.S.<strong>01</strong>489 FAA STC SA10365SC PIPER PA-31T<br />
PIPER PA-31T1<br />
FAA STC SA10365SC: Installation of a Benz<br />
Airborn System Model 800-0021 torque<br />
pressure system.<br />
1003<strong>04</strong>05 BENZ AIRBORNE SYSTEMS FAA STC SA<strong>01</strong>969CH DHC-6-100, -200, -300 Installation of Torque Pressure System on<br />
DHC-6 in acc. to FAA STCSA<strong>01</strong>969CH<br />
1003<strong>04</strong>08 BENZ AIRBORNE SYSTEMS FAA STC SA<strong>01</strong>970CH DHC-6-100, -200, -300 Installation of Engine Oil Pressure System on<br />
DHC-6 in acc. to FAA STCSA<strong>01</strong>970CH<br />
10029629 BERINGER AERO PC-6/A2-H2, PC-6/B1-H2<br />
PC-6/B2-H2, PC-6/B2-H4<br />
BRGAP-STC-002 - New wheels and brake<br />
system.<br />
<strong>04</strong>.09.2<strong>01</strong>2<br />
N/A 19.03.2007<br />
For models DHC-6-100 and DHC-6-200, this<br />
installation is only applicablewhen the airplane<br />
has been modified with PT6A-27 engines.<br />
For models DHC-6-100 and DHC-6-200, this<br />
installation is only applicablewhen the airplane<br />
has been modified with PT6A-27 engines.<br />
Prior to installation of this modification it 15.06.2<strong>01</strong>0<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 />
Prior to installation of this modification it 15.06.2<strong>01</strong>0<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 />
None. Prior to installation of this modification the 08.<strong>04</strong>.2<strong>01</strong>0<br />
installer must determinethat the<br />
interrelationship between this modification<br />
and any otherpreviously installed<br />
modification will introduce no adverse<br />
effect uponthe airworthiness of the<br />
product.<br />
None None 10.10.2<strong>01</strong>2<br />
10<strong>04</strong>1707 BERINGER AERO DISCUS-2A, DISCUS A,<br />
BRGAP-STC-007(0) - Replacement of wheel<br />
VENTUS-2A, VENTUS A. and brake system<br />
10<strong>04</strong>2599 BERINGER AERO 1- DHC-6 SERIES 1<br />
Replacement of nose wheel BF Goodrich 8.90- None. Prior to installation of this modification it 10.12.2<strong>01</strong>2<br />
1- DHC-6 SERIES 100<br />
12.5 P/N 3-1197 by Beringerwheel assembly<br />
must be determined thatthe<br />
1- DHC-6 SERIES 110<br />
P/N: RA-008.<br />
interrelationship between this modification<br />
1- DHC-6 SERIES 200<br />
and any other previouslyinstalled<br />
1- DHC-6 SERIES 210<br />
modification and/ or repair will introduce<br />
1- DHC-6 SERIES 300<br />
no adverse effectupon the airworthiness<br />
1- DHC-6 SERIES 310<br />
1- DHC-6 SERIES 320<br />
2- DHC-6 SERIES 400<br />
of the product.<br />
10036735 BHE & ASSOCIATES, LTD. B200, B200C, B200CGT, B200GT Installation of upgraded hardware to the This Installation is limited to aircraft serials Prior to installation of this modification it 05.10.2<strong>01</strong>1<br />
B300, B300C<br />
Rockwell Collins Pro Line 21FMS-3000 to listed in BHE andAssociates document 324-00- must be determined thatthe<br />
provide Localiser Performance with Vertical 0002, Rev IR, dated November 24, 2009, interrelationship between this modification<br />
Guidance (LPV).<br />
orlater approved revisions.<br />
and any other previouslyinstalled<br />
modification and/ or repair will introduce<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
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