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>6811 ONBOARD SYSTEMS INTERNATIONAL <strong>EASA</strong>.IM.R.S.<strong>01</strong>171 REV. 1 FAA STC SR<strong>01</strong>064SE ROBINSON R44<br />
Cargo hook suspension system i.a.w. US STC This STC is approved only for the product<br />
29.<strong>04</strong>.2009<br />
ROBINSON R44 II<br />
SR0<strong>01</strong>064SE.Note: Revision 1 of this STC is configuration as defined in the approved design<br />
made for correction of FAA original STC data referred to in the paragraph "Description".<br />
reference. This supersedes previous issuance Compatibility with other aircraft/engine<br />
of the STC.<br />
configurations shall be determined by the<br />
installer.<br />
10<strong>01</strong>6862 ONBOARD SYSTEMS INTERNATIONAL <strong>EASA</strong>.IM.R.S.<strong>01</strong>238 FAA STC SR<strong>01</strong>164SE EUROCOPTER FRANCE AS 350 Fabrication and Installation of Onboard 1. Approval of this change in Type Design<br />
26.07.2006<br />
B<br />
Systems Model 200-280-<strong>01</strong> Cargo Hook Swing applies only fo those Eurocopter AS350 model<br />
EUROCOPTER FRANCE AS 350 Suspension System<br />
rotorcraft listed above;2. This approval<br />
B1<br />
should not be extended to other rotorcraft of<br />
EUROCOPTER FRANCE AS 350<br />
these models on which other previously<br />
B2<br />
EUROCOPTER FRANCE AS 350<br />
B3<br />
EUROCOPTER FRANCE AS 350<br />
BA<br />
EUROCOPTER FRANCE AS 350<br />
D<br />
approved modifications areincorporate<br />
10<strong>01</strong>6869 ONBOARD SYSTEMS INTERNATIONAL <strong>EASA</strong>.IM.R.S.<strong>01</strong>245 FAA STC SR00649SE BELL 206A<br />
Cargo Hook Suspension Kit for Bell 206A and None 21.12.2006<br />
BELL 206B<br />
206B<br />
10<strong>01</strong>6870 ONBOARD SYSTEMS INTERNATIONAL <strong>EASA</strong>.IM.R.S.<strong>01</strong>246 REV. 1 FAA STC SR<strong>01</strong>393SE AS350B, AS350BA, AS350B1 Onboard Systems cargo hook kits P/N 200-286-None<br />
This STC is approved only for the product <strong>04</strong>.02.2<strong>01</strong>1<br />
AS350B2, AS350B3, AS350D <strong>01</strong> (with cargo hook P/N528-023-<strong>01</strong>) and P/N<br />
configuration as defined inthe approved<br />
200-286-02 (with cargo hook P/N 528-029-<br />
design data referred to in the paragraphs<br />
00)Revision 1 - introduces cargo hook kit P/N<br />
"Title/Description" and "Associated<br />
200-286-02This STC is the validation of FAA<br />
Technical Documentation". Compatibility<br />
STC SR<strong>01</strong>393SE (issued on April 05,20<strong>04</strong><br />
with other aircraft/engine configurations<br />
shall bedeterm<br />
10<strong>01</strong>6874 ONBOARD SYSTEMS INTERNATIONAL <strong>EASA</strong>.IM.R.S.<strong>01</strong>250 FAA STC SR00920SE ROBINSON R22<br />
ROBINSON R22 ALPHA<br />
ROBINSON R22 BETA<br />
ROBINSON R22 MARINER<br />
Cargo Hook Suspension Kit i.a. with FAA STC<br />
SR00920SE<br />
10<strong>01</strong>6907 ONBOARD SYSTEMS INTERNATIONAL <strong>EASA</strong>.IM.R.S.<strong>01</strong>287 FAA STC SR00711SE SCHWEIZER 269 SERIES Validation of FAA STCSR00711SE , amended<br />
January 13, 2003, or later approved versions.<br />
10<strong>01</strong>6937 ONBOARD SYSTEMS INTERNATIONAL <strong>EASA</strong>.IM.R.S.<strong>01</strong>324 REV. 2 FAA STC SR<strong>01</strong>164SE AS 350 B, AS 350 B1<br />
AS 350 B2, AS 350 B3<br />
AS 350 BA, AS 350 D<br />
10<strong>01</strong>6990 ONBOARD SYSTEMS INTERNATIONAL <strong>EASA</strong>.IM.R.S.<strong>01</strong>396 REV. 1 FAA STC SR0<strong>04</strong>07SE MD HELICOPTERS 369D<br />
MD HELICOPTERS 369E<br />
MD HELICOPTERS 369F<br />
MD HELICOPTERS 369FF<br />
MD HELICOPTERS 369HE<br />
MD HELICOPTERS 369HM<br />
MD HELICOPTERS 369HS<br />
MD HELICOPTERS 500N<br />
10<strong>01</strong>6993 ONBOARD SYSTEMS INTERNATIONAL <strong>EASA</strong>.IM.R.S.<strong>01</strong>402 FAA STC SR<strong>01</strong>795SE EUROCOPTER FRANCE EC 120<br />
B<br />
10<strong>01</strong>6999 ONBOARD SYSTEMS INTERNATIONAL <strong>EASA</strong>.IM.R.S.<strong>01</strong>409 FAA STC SR<strong>01</strong>778SE MD HELICOPTERS 369D<br />
MD HELICOPTERS 369E<br />
MD HELICOPTERS 369F<br />
MD HELICOPTERS 369FF<br />
MD HELICOPTERS 369HE<br />
MD HELICOPTERS 369HM<br />
MD HELICOPTERS 369HS<br />
MD HELICOPTERS 500N<br />
-- 20.12.2006<br />
Approval of this STC apply only to those<br />
Schweizer 269C which were previously<br />
equipped with FAA approved installation of<br />
Schweizer cargo hook kit P/N 269A4971-<br />
27.Modified rotorcraft must be operated i.a.w.<br />
FAA approved Rotorcraft Flight manual<br />
09.07.2007<br />
External Load Swing Suspension System<br />
Supplement (<br />
1. <strong>EASA</strong>-approved AS350 Flight Manual Prior to installation of this modification it 21.06.2<strong>01</strong>0<br />
models 200-280-<strong>01</strong> and -<strong>04</strong> (withKeeperless and must be determined thatthe<br />
Cargo Hooks) and model 200-280-02 and -03 FM supplement are required.2. This STC is interrelationship between this modification<br />
(with HydraulicCargo Hooks) Revision 1 - approved only for the product configuration as and any other previouslyinstalled<br />
introduced cargo hook kit 200-280-03 with a defined inthe approved design data referred to modification and/ or repair will introduce<br />
collectivefriction knob and a new release lever t in the paragraph "Description".Compatibil no adverse effectupon the airworthiness<br />
of the product.<br />
Onboard Systems Model 200-187-00 cargo Approval of this change in type design applies<br />
hook on helicopters 369D, 369E, 369FF. to only those McDonnell Douglas model<br />
369HE, 369HM, 369HS, 500N<strong>EASA</strong> validation rotorcraft listed above, which were<br />
of FAA STC SR0<strong>04</strong>07SE , amended 2 previouslyequipped with an FAA approved<br />
October 2007, or later approved 07This STC is installation of McDonnell Douglas cargo hook<br />
classified ‘Basic’ by the FAA and is approved suspension systems and Breeze-Eastern cargo<br />
under the po<br />
hooks<br />
Installation of Cargo Hook Suspension Kit P/N<br />
200 - 308 – 00.<br />
1. All limitations of RFM supplement apply;2.<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 effec<br />
Onboard Systems Model 200-300-00 talon LC This cargo hook is not approved for human<br />
Hydraulic Cargo Hook Kit without load weight, external loadApproval of this change in type<br />
Model 200-3<strong>01</strong>-00 talon LC Hydraulic Cargo design applies to only those McDonnell<br />
Hook Kit with load weight on helicopters 369D, Douglas model rotorcraft listed above, which<br />
369E, 369FF. 369HE, 369HM, 369HS, 500N were previouslyequipped with • Onboard<br />
system model 200-187-00 cargo hook<br />
(approva<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 350/<strong>462</strong><br />
18.03.2008<br />
22.<strong>01</strong>.2008<br />
08.07.2008
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