This test report describes the test results of the below mentioned paragliding harness. Sup'Air Kinder S 2.1 kg 100 kg ABS
|
|
- Gabriel Long
- 6 years ago
- Views:
Transcription
1
2 Test Report This test report describes the test results of the below mentioned paragliding harness. All the tests were carried out by: Air Turquoise SA, official test laboratory of Switzerland. Standards Tests were carried out in conformity with the following standards: 2. DV LuftGerPV 1, Nr. 7 c (*note: in what follows this will be abbreviated by LTF ) European Standard EN1651 September 1999 (*note in what follows this will be abbreviated by EN ) European Standard EN12491 September 2001 (*note in what follows this will be abbreviated by EN12491 ) Harness details : Harness model: Size: Harness Weight: Maximum certified pilot Impact protection type: Harness type: S 2.1 kg Mousse bag ABS Test place: Test date: Test room temp & humidity: Certification number EN: Certification number LTF: Villeneuve April 12, 2013 PH GZ page 1 of 4
3 Test summary A. STRUCTURAL STRENGHT TESTS A test plan was set up in order to execute the different tests in an efficient order. The table below summarizes this test plan together with the applicable standards and results. Test ID g Default 2 main 10 OK a flying attachment Hip fixated 9g 9000 position points g OK 3 Default, b 2 main att. Hip fixated, 6g OK landing points position landing conf. 15g OK a 5 rescue 9g n/a Rescue Hip fixated rescue att. 15g n/a Pnts b Rescue, Hip fixated, 7 6g n/a rescue landing landing conf. ONE main att d 3g Towing 2 main att. + None 10 n/a tow att. 5g Standard Ref. EN LTF Dummy Req. Min. Attach - ment points Load in g force [N] One riser TESTED? Default, Negatif Upside c 2 main att. down downw c rescue TEST setup Upside down rescue Anchoring 1 central hip fixation One main att. Head fix. 4.5g OK 2 rescue att. downw. Head fix. Forces Min. Test durat ion [sec] Result 6g OK 6g OK 6g n/a B. HARNESS PROTECTION SHOCK TEST Most paraglider harnesses are equipped with a protection device that damps the shock on the pilot s spine during a hard landing. Shock impact tests have to be executed on these harnesses in order to prove the damping characteristics of it. page 2 of 4
4 Test ID PRO TECT 1 TESTED? Standa rd Ref.: LTF TEST setup Default flying position Attachment points Anchoring Dummy Test dummy is attached to the harness like a pilot in flight. Max. tolerated peak impact in g Impact Max Peak impact measured Impact duration of +38 g (if any) recorded: +50g g 6 ms Impact duration of +20 g (if any) recorded: Result 17 ms OK C. RESCUE DEPLOYMENT RESISTANCE TEST The deployment of the rescue system has to be ensured in all circumstances of flight. This test is to verify whether the force needed to deploy is in between reasonable limits. Test ID Resc depl TESTED? Standa rd Ref. LTF TEST setup Default flying position Anchoring Attachment Min. Max. force points force [N] [N] Test responisble is attached to the harness like a pilot in flight. 20 N 70 N Dummy (no dummy required) Force for single hand deployment Resistance measured [dan] n/t Result n/a D. RESCUE DEPLOYMENT STRAP STRENGHT TEST The connection between handgrip and inner container has to have sufficient load capacity/structural strength in any situation that may arise during normal use. During this test is verified, whether this connection fulfill the requirements. Test ID TESTED? Standard Ref. TEST setup Min. Test durati on LTF EN Minimum force [N] [s] Breaking resistance measured Result Resc strap Connection strap in tensile testing machine 700N 10 n/t n/a page 3 of 4
5
6 Annex: detailed test reports Harness Test Test ID 1 Standard EN 1651 & 2. DV LuftGerPV 1, Nr. 7 c Test standard : (EN) & a (LTF DV) Default flying position Anchoring: Attachment points: Both main riser attachments (3, 4) Dummy: Default, hip fixed (7, 8) Required load in g : 9g (EN: 6g) Minimum load [N]: 9000 N (EN: 6000 N) Required test load in kg: 900 kg Min. duration [s]: 10 s Duration of maintained min. load [s]: 10.9 s Any signs of structural failure after this test: Test result: No visible failure Graph: 1200 TEST ID 1: EN & LTF a Norm 600 dan norm 900 dan 1000 Force (dan) Annex TEST ID 1
7 Harness Test Test ID 2 Standard EN 1651 Test standard : Default flying position Anchoring: Attachment points: Both main riser attachments (3, 4) Dummy: Default, hip fixed (7, 8) Required load in g: 15 g Min load [N]: N Required test load in kg: 1500 kg Min. duration [s]: 5s Duration of maintained min. load [s]: 6.7 s Any signs of structural failure after this test: Test result: No visible failure Graph: TEST ID 2: EN Norm 1500 dan Force (dan) Annex TEST ID 2
8 Harness Test Test ID 3 Standard Test standard : 2. DV LuftGerPV 1, Nr. 7 c b Anchoring: Attachment points: Dummy: Flying position before landing: seat board (11) in landing position, leg straps (10) closed. Both of the main riser attachments attached (3 and 4); Default, hip fixed (7, 8) Required load in g: 6 g Min load [N]: 6000 N Required test load in kg: 600 kg Min. duration [s]: 10 s Duration of maintained min. load [s]: 10.3 s Any signs of structural failure after this test: Test result: No visible failure Graph: TEST ID 3: LTF b Norm 600 dan Force (dan) Annex TEST ID 3
9 Harness Test Test ID 4 Standard EN 1651 Test standard : EN Anchoring: Attachment points: Dummy: Flying position before landing: seat board (11) in landing position, leg straps (10) closed. Both of the main riser attachments attached (3 and 4); Default, hip fixed (7, 8) Required load in g: 15 g Min load [N]: N Required test load in kg: 1500 kg Min. duration [s]: 5 s Duration of maintained min. load [s]: Any signs of structural failure after this test: No visible failure Test result: Graph: TEST ID 4: EN Norm 1500 dan Force (dan) Annex TEST ID 4
10 Harness Test Test ID 8 Standard EN 1651 Test standard : Only one riser attached Anchoring: Attachment points: One main riser attachments (3) Dummy: Hip fixed (7, 8 -> 12) Required load in g: 6 g Min load [N]: N Required test load in kg: 600 kg Min. duration [s]: 10 s Duration of maintained min. load [s]: 11.1 s Any signs of structural failure after this test: Test result: No visible failure Graph: 800 TEST ID 8: EN Norm 600 dan Force (dan) Annex TEST ID 8
11 Harness Test Test ID 10 Standard EN 1651 Test standard : Normal flying position in NEGATIF Anchoring: Attachment points: Dummy: Required load in g: Min load [N]: 4.5 g Required test load in kg: 450 kg Min. duration [s]: ONE of the main riser attachments attached downwards(3 or 4); Dummy anchored at the head position (9) 4500 N 10 s Duration of maintained min. load [s]: 11.8 s Any signs of structural failure after this test: No visible failure Test result: Graph: TEST ID 10: EN Norm 450 dan Force (dan) Annex TEST ID 10
12 Harness Test Test ID 11 Standard Test standard : 2. DV LuftGerPV 1, Nr. 7 c c Pilot upside down flying position Anchoring: Attachment points: Dummy: Required load in g: Min load [N]: 6 g N Required test load in kg: 600 kg Min. duration [s]: 10 s Both of the main riser attachments attached downwards (3 and 4); Dummy anchored at the head position (9) Duration of maintained min. load [s]: 11.9 s Any signs of structural failure after this test: Test result: No visible failure Graph: 700 TEST ID 11: LTF c Norm 600 dan Force (dan) Annex TEST ID 11
13 Protector shock test Test ID Protect Standard 2. DV LuftGerPV 1, Nr. 7 c Test standard : Requirements: Minimun height: Impact requirements: Repetitions: Harness attached to protector test dummy, in a similar way like a real pilot in flight. Impact will be simulated by dropping the dummy from a certain height (with and without reserve). To simulate the in-flight conditions, the airbag is inflated with pressurized air equalling an airspeed of 7m/s. Inflation has to be stopped at least 5 sec before impact. Impact will be measured by an accelerometer mounted on the dummy. (Impact measured in g s) 1.65 m (between lowest point test dummy and impact surface) +50g as absolute maximum; +38g during less than 7 msec; +20g during less than 25 msec. The test will be performed 2 times, minimum 1 hour and maximum 2 hours after the first impact (with airbag protectors this pause is not necessary). The 2 Max-values should not differ more than 20% Shock test 1: Impact at a height of 1.65m: Impact duration of+ 38 g (if any): Impact duration of +20 g (if any): g 6 ms 17 ms < 20 %? Shock test 2: Impact at a height of 1.65m: Impact duration of+ 38 g (if any): Impact duration of +20 g (if any): g 4.1 ms 16.9 ms Test Result: Annex TEST ID Protect 1
14 Graph 1: TEST ID PROTECT: LTF Norm +50g Norm +38g Norm +20g Decelaration in g's Graph 2: TEST ID PROTECT: LTF Norm +50g Norm +38g Norm +20g Decelaration in g's Annex TEST ID Protect 1
This test report describes the test results of the below mentioned paragliding harness. Dudek Paragliders Pogo 2 Medium 5.
Test Report This test report describes the test results of the below mentioned paragliding harness. All the tests were carried out by: Air Turquoise SA, official test laboratory of Switzerland. s Tests
More informationThis test report describes the test results of the below mentioned paragliding harness. Ozone Gliders Exoceat Medium 7.
Test Report This test report describes the test results of the below mentioned paragliding harness. All the tests were carried out by: Air Turquoise SA, official test laboratory of Switzerland. Standards
More informationThis test report describes the test results of the below mentioned paragliding harness. Sup'Air Evo XC 3 Large 4.2 kg 120 kg Mousse bag ABS
Test Report This test report describes the test results of the below mentioned paragliding harness. All the tests were carried out by: Air Turquoise SA, official test laboratory of Switzerland. Standards
More informationThis test report describes the test results of the below mentioned paragliding harness.
Test Report This test report describes the test results of the below mentioned paragliding harness. All the tests were carried out by: Air Turquoise SA, official test laboratory of Switzerland. Standards
More informationThis test report describes the test results of the below mentioned paragliding harness. SUPAIR - VLD Delight 2 Medium 2.5 kg 120 kg Foam 15 cm ABS
Test Report This test report describes the test results of the below mentioned paragliding harness. All the tests were carried out by: Air Turquoise SA, official test laboratory of Switzerland. Standards
More informationThis test report describes the test results of the below mentioned paragliding harness.
Test Report This test report describes the test results of the below mentioned paragliding harness. All the tests were carried out by: Air Turquoise SA, official test laboratory of Switzerland. Standards
More informationThis test report describes the test results of the below mentioned paragliding harness. Ozone Gliders Ozium Medium 1.
Test Report This test report describes the test results of the below mentioned paragliding harness. All the tests were carried out by: Air Turquoise SA, official test laboratory of Switzerland. Standards
More informationThis test report describes the test results of the below mentioned paragliding harness. SUP'AIR Walibi 2 Medium 3.3 kg 100 kg Air bag ABS
Test Report This test report describes the test results of the below mentioned paragliding harness. All the tests were carried out by: Air Turquoise Para-test, official test laboratory of Switzerland Standards
More informationThe under mentioned sam pie of paraglider harness has been tested successfully in accordance with following standards: M ed iu m. 3.
para-test.com r r' C 1 ~,~J( Air TUfquoise SA Rte du Pré-au-Comte 81 CH-I8Ul.I Vlleneuve lei. UI 21 9656565 1 mobile.ul 79 22 52 3 IntcllJaara-test.com Mr. Nemec Martin Okruzni 39 73911 FrYdlant nad Ostravici
More informationProduct presentation
Product presentation SUCCESS 4 Comfort and Safety at its best Super safe, very comfortable, and sporty: The SUCCESS 4 is much more than another revamp of the popular SUCCESS series. This sports harness
More informationCanopy dimensions REPORT CCC 1
Canopy dimensions REPORT CCC 1 est report ref. number: CCC-018.2017 OZONE - ENZO 3 XS Name: Enzo 3 Place: Villeneuve Manufacturer name: Ozone Gliders Paragliders permitted in FAI Category 1 Cross-Country
More informationEuropean Aviation Safety Agency
TCDS.R.123 Page 1 of 22 European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET SE 3160 SA 316B SA 316C SA 319B SA 315B Type Certificate Holder: Eurocopter Aéroport International Marseille Provence
More informationProposal. Submitted. agenda item 17) supersedes made 2017/04/19) Insert new. of the. The minimum size area." Insert new. inform the.
Submitted by the expert from France Informal document GRSP-61-15-Rev.11 (61 st GRSP, 08-12 May 2017 agenda item 17) Proposal for Supplement 3 to the 01 series of amendments to Regulation No. 129 Submitted
More informationTEST REPORT FOR: Product Design Group Inc. Elevation Manual Wheelchair 115 kg, 253 lb
TEST REPORT FOR: Product Design Group Inc. Elevation Manual Wheelchair 115 kg, 253 lb REFERENCED DOCUMENTS ISO7176-1:1999, ISO7176-3:2003, ISO7176-5:2008, ISO7176-7:1998, ISO7176-8:1998, ISO7176-13:1989
More informationContact person Date Reference Page Mikael Videby P08110A 1 (6) SP Structural and Solid Mechanics
issued by an Accredited Testing Laboratory Contact person Mikael Videby 2015-11-13 5P08110A 1 (6) SP Structural and Solid Mechanics +46 10 516 50 36 Mikael.Videby@sp.se Accred. No. 1002 Testing ISO/IEC
More informationWP5 - Computational Mechanics B5 - Temporary Vertical Concrete Safety Barrier MAIN REPORT Volume 1 of 1
ROBUST PROJECT TRL Limited WP5 - Computational Mechanics B5 - Temporary Vertical Concrete Safety Barrier MAIN REPORT Volume 1 of 1 December 2005 Doc. No.: ROBUST-5-010c Rev. 0. (Logo here) Main Report
More informationTYPE-CERTIFICATE DATA SHEET
Issue: 02 Date: 27 October 2017 TYPE-CERTIFICATE DATA SHEET NO. EASA. A.616 for Type Certificate Holder M&D Flugzeugbau GmbH & Co. KG Streeker Straße 5 b 26446 Friedeburg Germany For models: JS-MD 1C TE.CERT.00135-001
More informationTYPE-CERTIFICATE DATA SHEET
TYPE-CERTIFICATE DATA SHEET NO. EASA.A.616 for Type Certificate Holder M&D Flugzeugbau GmbH & Co. KG Streeker Straße 5 b 26446 Friedeburg Germany For models: JS-MD 1C TE.CERT.00135-001 European Union Aviation
More informationE/ECE/324/Rev.2/Add.128/Rev.2/Amend.2 E/ECE/TRANS/505/Rev.2/Add.128/Rev.2/Amend.2
10 August 2018 Agreement Concerning the Adoption of Harmonized Technical United Nations Regulations for Wheeled Vehicles, Equipment and Parts which can be Fitted and/or be Used on Wheeled Vehicles and
More informationPENTAGON PROTECTION USA
PENTAGON PROTECTION USA Shock Tube Testing for Window Systems March 2009 San Antonio, Texas ABS Consulting Project Number 2127174 ABSG Consulting, Inc. 14607 San Pedro, Suite 215 San Antonio, TX 78232
More informationGuidelines for the Noise Measurement of Homebuilt Aircraft
Guidelines for the Noise Measurement of Homebuilt Aircraft ANCAT Ad Hoc Group on Noise Measurement of Homebuilt Aircraft European Civil Aviation Conference 7 May 2013 Guidelines for the Noise Measurement
More informationDISPOSAL OF STEERING WHEEL PAD (WITH AIRBAG)
AB82 DISPOSAL OF STEERING WHEEL PAD (WITH AIRBAG) When scrapping vehicles equipped with an airbag system or disposing of a steering wheel pad (with airbag), always first deploy the airbag in accordance
More informationCertificate of testing
Manufacturer: Roltec A/S Lægårdsvej 13 DK-8520 Lystrup, Denmark Page 1 of 9 Certificate of testing Crash Test according to ISO 10542-5 Wheelchair tiedown and occupant-restraint systems. Systems for specific
More informationAGATE (ADVANCED GENERAL AVIATION TRANSPORTATION EXPERIMENT PROGRAM) FULL-SCALE TEST AND DEMONSTRATION REPORT NO: C-GEN (REV N/C)
AGATE (ADVANCED GENERAL AVIATION TRANSPORTATION EXPERIMENT PROGRAM) FULL-SCALE TEST AND DEMONSTRATION REPORT NO: C-GEN-3451-1 (REV N/C) AGATE RESTRICTED INFORMATION This document contains information developed
More informationTYPE CERTIFICATE DATA SHEET
TYPE CERTIFICATE DATA SHEET No. EASA.IM.R.003 for Type Certificate Holder Erickson Incorporated, DBA Erickson Air-Crane 3100 Willow Springs Road P.O. Box 3247 Central Point, Oregon, 97502-0010 U.S.A. For
More informationSENTINEL-1 SAR DEM DEPLOYMENT MECHANISMS RECOVERY
SENTINEL-1 SAR DEM DEPLOYMENT MECHANISMS RECOVERY Laura Rivera (1),Carlos Compostizo (1), Ibon Arregui (1) (1) SENER, Av. Zugazarte 56, 48930 Las Arenas (Bizkaia) Spain, Email: laura.rivera@sener.es ABSTRACT
More informationService Bulletin A
THOR-50M Euro NCAP SBL-A Update Publication Date: January 207 Humanetics now offers the THOR-50M Standard Build Level A (SBL-A) which is intended to meet the drawings and qualification specifications defined
More informationDevelopment of the Japan s RDE (Real Driving Emission) procedure
Informal document GRPE-76-18 76 th GRPE, 9-12 January 2018 Agenda item 13 Development of the Japan s RDE (Real Driving Emission) procedure Environmental Policy Division, Road Transport Bureau, Ministry
More informationCoolers. OK Series. Air Cooled Oil Coolers Hydraulic Symbol OK 1-11 OKF Cooling Systems Catalog. Applications
OK Series Air Cooled Oil Coolers Hydraulic Symbol OK 1-11 OKF 3-11 OKA 4-6 OKAF 4-6 OKA 8-11 OKAF 8-11 Description The OK Series cooler design uses a axial fan assembly which draws air through the cooler.
More informationJRS Dynamic Rollover Test Chevrolet Malibu
Page 1 of 61 JRS Dynamic Rollover Test 2009 Chevrolet Malibu Sponsored By: Automotive Safety Research Institute Charlottesville, VA. Vehicle Donated by: State Farm Insurance Company Chicago, IL. Introduction
More informationTest Report No
Empa Überlandstrasse 129 CH-8600 Dübendorf Tel. +41 (0)44 823 55 11 Fax +41 (0)1 821 62 44 www.empa.ch Materials Science & Technology Lista AG Betriebs- und Lagereinrichtungen CH-8586 Erlen Test Report
More informationNovitaTech Engineering
NovitaTech Engineering 490869 TEST REPORT FOR PDG Product Design Group Eclipse 600 MANUAL WHEELCHAIR TEST DOCUMENTS AS3695:1992, AS3696-1:1990, AS 3696-3:1990, AS 3696-5:1989, AS 3696-8:1998, ISO 7176-7:1996
More informationThe Highest Quality Heavy Duty Vehicular Electrical Switches and Components at Competitive Prices
The Highest Quality Heavy Duty Vehicular Electrical Switches and Components at Competitive Prices UCOM INC was created in 1994 to fill a specific niche in the marketplace. We specialize in providing the
More informationTYPE-CERTIFICATE DATA SHEET
TYPE-CERTIFICATE DATA SHEET No. E. 103 Issue 2 for ARDIDEN 3 series engines Type Certificate Holder Avenue Joseph Szydlowski 64510 Bordes France For Models: ARDIDEN 3G ARDIDEN 3C TE.CERT.00052-001 European
More informationTESTING REPORT. ROLLATORS - ISO classification in accordance with the INTERNATIONAL STANDARD ISO :2005. Testing No. 07.
Danish Centre for Assistive Technology TESTING REPORT ROLLATORS - ISO classification 12.06.06 in accordance with the INTERNATIONAL STANDARD ISO 11199-2:2005 Testing No. 07.44A This page is page 1 of a
More informationTYPE-CERTIFICATE DATA SHEET
TYPE-CERTIFICATE DATA SHEET No. IM.E.016 issue 10 for FJ44/FJ33 Series Engines Certificate Holder Williams International Co. Walled Lake Michigan 48390-0200 USA For Models: FJ44-1A FJ44-1AP FJ44-2A FJ44-2C
More informationTEST REPORT FOR: Product Design Group Fuze T50 Manual Wheelchair (204 kg / 450 lb)
TEST REPORT FOR: Product Design Group Fuze T50 Manual Wheelchair (204 kg / 450 lb) REFERENCED DOCUMENTS ISO7176-1:1999, ISO7176-3:2003, ISO7176-5:2008 ISO7176-7:1998, ISO7178-8:1998, ISO7176-13:1989, ISO7176-15:1996,
More informationEuropean Aviation Safety Agency
Issue 16, 15 July, 2015 European Aviation Safety Agency EASA TYPE CERTIFICATE DATA SHEET AB139 (from S/N 31001 up to S/N 31054) Name changed in AW139 (from S/N 31055 onwards) Type Certificate Holder: AGUSTAWESTLAND
More informationCONTINUOUS IMMERSION AND DUST TEST REPORT
Report No. :HS1404020081A Version:A CONTINUOUS IMMERSION AND DUST TEST REPORT Company Address :Taiway Electronics Components Co. :4F., No. 4, 6, 8, Lane 359, Sec. 2, Zhongshan Rd., Zhonghe Dist., New Taipei
More informationCircuit Breakers. Switching & Controls. Selection Guide NC1V Series Dimensions...
Switching & ontrols Selection Guide... 1028 1V Series... 1029 Dimensions... 1035 www.ide.com/circuitbreaker ircuit Breakers Switches & Pilot Lights Signaling Lights Relays & Sockets Timers ontactors Terminal
More informationTest report P E. J. Magner Dipl.-Ing. (FH) N. Machill
Kiwa Polymer Institut GmbH Quellenstraße 3 D-65439 Flörsheim-Wicker Tel. +49 (0)61 45-5 97 10 Fax +49 (0)61 45-5 97 19 www.kiwa.de Test report P 8464-2-E Testing order: Tests on the coating Wecryl 124
More informationCOMMENT RESPONSE DOCUMENT
EASA COMMENT RESPONSE DOCUMENT EASA PSC No. SC-OVLA.div-01 [Published on the 13-April-2010 and officially closed for comments on the 01-July-2010] Commenter 1 :AD&C date 17-May-2010 In the proposed Special
More informationInvestigation Report.
Investigation Report. Status: Final Date: 27 JAN 08 Time: 11.30 UT Type: Piper PA 18-150 (180 HP) Operator: Royal Verviers Aviation Registration: OO-OAW C/N : 4828 msn : 18-5346 Manufacturing Date: 1957
More informationTYPE-CERTIFICATE DATA SHEET
TYPE-CERTIFICATE DATA SHEET No. E.001 For Models: B B1 B1A B1B D C C1 C S1 S E N H for Series Engines Type Certificate Holder 64510 Bordes France TE.CERT.0005-001 European Aviation Safety Agency, 018.
More informationJoint Australian and Canadian Pole Side Impact Research
Joint Australian and Canadian Pole Side Impact Research Thomas Belcher Australian Government Department of Infrastructure and Transport Suzanne Tylko Transport Canada 7 th Meeting - GRSP Informal Group
More informationRev E BearPaw Model BP44 Installation Instructions - R44/R66
TABLE OF CONTENTS: INTRODUCTION p.2 Scope p.2 General p.2 Helicopter Effectivity p.2 Installer Responsibilities p.2 INSTALLATION p.3 BearPaw Installation p.3 BearPaw Removal p.4 Weight & Balance p.5 Parts
More informationTest Report Project Nr. 2013/020
PISTON Ltd. 1033 Budapest Szőlőkert u. 4./B HUNGARY Tel: Fax: http: Email: (361)-275-0033 (361)-275-0034 www.pistonmedical.com info@pistonmedical.com Test Report Project Nr. 2013/020 Name and address of
More informationPTV TECHNICAL PRESCRIPTIONS. ELASTOMERIC SEALS: Part 1: Vulcanized Rubber FOR. Impartial institute for the monitoring of construction products
PTV 8681-1 TECHNICAL PRESCRIPTIONS TECHNICAL PRESCRIPTIONS FOR ELASTOMERIC SEALS: Part 1: Vulcanized Rubber COPRO vzw Version 1.0 dated 2017-10-17 Impartial institute for the monitoring of construction
More informationDKG-114 MANUAL AND REMOTE START UNIT
DKG-114 MANUAL AND REMOTE START UNIT FEATURES Both manual and remote controlled engine starting and stopping, Automatic shutdown on fault condition, Optional cooldown cycle on remote start operation, Optional
More informationResearch TEST Result. Japanese Proposal
GRSP Inf. Group on on a Pole Side Impact GTR PSI-05-06 March 22,23, 2012 Research TEST Result & Japanese Proposal JASIC / Japan Background Though number of pole side impact accidents is small, the fatal
More informationEuropean Aviation Safety Agency
European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET Schleicher ASW 28 Manufacturer: Alexander Schleicher GmbH & Co Segelflugzeugbau Models: ASW 28 ASW 28-18 Page 1 2 3 4 5 6 7 Issue 1 1 1
More informationAirworthiness Directive
Airworthiness Directive AD No.: 2018-0109 Issued: 17 May 2018 Note: This Airworthiness Directive (AD) is issued by EASA, acting in accordance with Regulation (EC) 216/2008 on behalf of the European Union,
More informationTYPE-CERTIFICATE DATA SHEET
TYPE-CERTIFICATE DATA SHEET EASA.IM.A.081 for Type Certificate Holder: PACIFIC AEROSPACE Ltd 333 Airport Road, Hamilton 3282, New Zealand For models: TE.CERT.00048-001 European Aviation Safety Agency,
More informationDiag. Code 13 Short in Squib Circuit (Between D+ Wire Harness and D Wire Harness)
SRS AIRBAG AB49 Diag. Code 13 Short in Squib Circuit (Between D+ Wire Harness and D Wire Harness) CIRCUIT DESCRIPTION The squib circuit consists of the center airbag sensor assembly, spiral cable and the
More informationSAFETY COMPLIANCE TESTING FOR FMVSS NO. 225 CHILD RESTRAINT ANCHORAGE SYSTEMS LOWER AND TETHER ANCHORAGES
REPORT NUMBER 225-GTL-06-006 SAFETY COMPLIANCE TESTING FOR FMVSS NO. 225 CHILD RESTRAINT ANCHORAGE SYSTEMS LOWER AND TETHER ANCHORAGES GENERAL MOTORS OF CANADA, LTD. 2005 BUICK LACROSSE, PASSENGER CAR
More informationAgenda. Introduction to IEC Differences between the 1 st and 2 nd edition. How will these changes impact the industry?
Agenda Introduction to IEC 62133 Scope Status Differences between the 1 st and 2 nd edition Brief overview of differences Changes to construction requirements Changes to tests for nickel cells and batteries
More informationAnti-Surge Thick Film Chip Resistors
FEATURES EXCELLENT ANTI-SURGE CHARACTERISTICS AEC-Q200 QUALIFIED RATED POWER UPGRADE IN SMALLER PACKAGE SIZE MEETS +85 C/85%RH TEST 000 HOURS MEETS CLIMATE CATEGORY (IEC 60068): 55/55/56 AVAILABLE IN ±
More informationCIRCUIT INSPECTION. DTC B0100/13 Short in D Squib Circuit CIRCUIT DESCRIPTION WIRING DIAGRAM
DI388 CIRCUIT INSPECTION DI18Q35 DTC B0100/13 Short in Circuit CIRCUIT DESCRIPTION The D squib circuit consists of the airbag sensor assembly, spiral cable and steering wheel pad. It causes the airbag
More informationTHE STRESS OF LASHING POINTS IN FULL- LOADED 3,5-TONNE VAN DURING EMERGENCY BRAKING
THE STRESS OF LASHING POINTS IN FULL- LOADED 3,5-TONNE VAN DURING EMERGENCY BRAKING Ján ZÁMEČNÍK, Juraj JAGELČÁK 1 Introduction and description of the tests During the emergency the forces occuring on
More informationAdelaide Wind Power Project Turbine T05 (AD117) IEC Edition 3.0 Measurement Report
REPORT ID: 14215.01.T05.RP6 Adelaide Wind Power Project Turbine T05 (AD117) IEC 61400-11 Edition 3.0 Measurement Report Prepared for: Suncor Adelaide Wind General Partnership Inc. 2489 North Sheridan Way
More informationJoint Research Centre
Joint Research Centre the European Commission's in-house science service Serving society Stimulating innovation Supporting legislation Overview of the Correlation and CO2MPAS Process J. Pavlovic, G. Fontaras,
More informationCIRCUIT INSPECTION. DTC B0100/13 Short in D Squib Circuit CIRCUIT DESCRIPTION WIRING DIAGRAM
DI254 CIRCUIT INSPECTION DI18Q37 DTC B0100/13 Short in Circuit CIRCUIT DESCRIPTION The D squib circuit consists of the airbag sensor assembly, spiral cable and steering wheel pad. It causes the airbag
More informationTYPE-CERTIFICATE DATA SHEET
TYPE-CERTIFICATE DATA SHEET NO. EASA.A.598 for Breezer B600 Certificate Holder Breezer Aircraft GmbH & Co. KG Sönke-Nissen-Koog 58 25821 Reußenköge Germany For models: B600 TE.CERT.000xx-001 European Aviation
More informationWP5 - Computational Mechanics B1 (ESP-N2) Barrier Steel N2 MAIN REPORT Volume 2 of 2
ROBUST PROJECT TRL Limited WP5 - Computational Mechanics B1 (ESP-N2) Barrier Steel N2 Volume 2 of 2 November 2005 Doc. No.: ROBUST 5-014b Rev. 1. (Logo here) Main Report Report title: WP5 - Computational
More informationSAFETY COMPLIANCE TESTING FOR FMVSS 202a Head Restraints
FINAL REPORT NUMBER 202a-MGA-10-003 SAFETY COMPLIANCE TESTING FOR FMVSS 202a FORD MOTOR COMPANY 2010 Lincoln MKT MPV NHTSA No. CA0213 MGA RESEARCH CORPORATION 446 Executive Drive Troy, Michigan 48083 Test
More informationAirworthiness Directive
Airworthiness Directive AD No.: 2016-0165 Issued: 12 August 2016 EASA AD No.: 2016-0165 Note: This Airworthiness Directive (AD) is issued by EASA, acting in accordance with Regulation (EC) 216/2008 on
More informationSKN_N0106AnnexJ_R2. Annex J - Specific requirements for PVT collector Certification. 1. Introduction and definition
Annex J - Specific requirements for PVT collector Certification 1. Introduction and definition PVT collectors (named hybrid collectors in ISO 9806) generate heat and electric power at the same time. They
More informationTowing Administration Introduction Towing Operations Weak Links Aerotow Pilot (ATP) Certification
Towing Administration Standard Operating Procedure 12-10 Last Amended March, 2017 12-10.01 Introduction This SOP outlines operating procedures for towing related sections of the Pilot Proficiency System
More informationTYPE-CERTIFICATE DATA SHEET
TYPE-CERTIFICATE DATA SHEET No. E.139 for Engine ASTAZOU II series engines Type Certificate Holder 64510 Bordes France For Models: ASTAZOU II A ASTAZOU II A2 TE.CERT.00052-001 European Aviation Safety
More informationEuropean Aviation Safety Agency EASA SPECIFIC AIRWORTHINESS SPECIFICATION. for. OA7 Optica Series 100/200/301
EASA.SAS.A.073 OA7 Optica Page 1 of 5 European Aviation Safety Agency EASA SPECIFIC AIRWORTHINESS SPECIFICATION for OA7 Optica Series 100/200/301 The UK Type Certificate for this aircraft type is no longer
More informationHumanetics is now shipping all ATDs for use in the U.S. NCAP at SBL-A and also offers upgrade kits for previously delivered dummies.
THOR-50M U.S. NCAP SBL-A Update Publication Date: January 07 Humanetics now offers the THOR-50M Standard Build Level A (SBL-A) which is intended to meet the drawings and qualification specifications defined
More informationCircuit Breakers. Switching & Controls. Selection Guide NC1V Series Dimensions Accessories
Switching & ontrols Selection Guide... 922 1V Series... 923 Dimensions... 929 Accessories... 932 ircuit Breakers Switches & Pilot Lights Signaling Lights Relays & Sockets Timers ontactors Terminal Blocks
More informationRoad vehicles Design and performance specifications for the WorldSID 50th percentile male side impact dummy Part 2: Mechanical subsystems
ISO 2011 All rights reserved ISO TC 22/SC 12 N Date: 2011-02-10 ISO TC 22/SC 12/WG 5 Secretariat: AFNOR Road vehicles Design and performance specifications for the WorldSID 50th percentile male side impact
More informationContact person Date Reference Page Michael Lindblad F000833F 1 (1) Sustainable Built Environment
issued by an Accredited Testing Laboratory Contact person Michael Lindblad 2015-06-25 5F000833F 1 (1) Sustainable Built Environment +46 10 516 58 58 Michael.Lindblad@sp.se 1002 ISO/IEC 17025 Martela AB
More informationSkid against Curb simulation using Abaqus/Explicit
Visit the SIMULIA Resource Center for more customer examples. Skid against Curb simulation using Abaqus/Explicit Dipl.-Ing. A. Lepold (FORD), Dipl.-Ing. T. Kroschwald (TECOSIM) Abstract: Skid a full vehicle
More informationSuccessful Deployment of ecall Live Crash Test
Successful Deployment of ecall Live Crash Test There is a growing necessity to conform to automotive safety regulations for emergency calls (ecalls). One popular car maker wanted to push its safety standards
More informationAirworthiness Directive
Airworthiness Directive AD No.: 2018-0211 Issued: 28 September 2018 Note: This Airworthiness Directive (AD) is issued by EASA, acting in accordance with Regulation (EU) 2018/1139 on behalf of the European
More informationGunnebo Lifting Offshore programme - accessories. High consistent quality generates long durability and safety
Gunnebo Lifting Offshore programme - accessories High consistent quality generates long durability and safety DNV 2.7-1 certificate We are certified by DNV to make type approval in 271 quality (Offshore
More informationCHECK AND CALIBRATION PROCEDURES FOR FATIGUE TEST BENCHES OF WHEEL
STANDARDS October 2017 CHECK AND CALIBRATION PROCEDURES FOR FATIGUE TEST BENCHES OF WHEEL E S 3.29 Page 1/13 PROCÉDURES DE CONTRÔLE ET CALIBRAGE DE FATIGUE BANCS D'ESSAIS DE ROUE PRÜFUNG UND KALIBRIERUNG
More informationAirplane wing test stand for simulating the airstream. Airbus Deutschland GmbH
Airplane wing test stand for simulating the airstream Airbus Deutschland GmbH 2 1 Airplane wing test stand for simulating the airstream Hänchen ist standard In test stands at Airbus in Bremen, Hänchen
More informationHIGH LOAD LOW SHOCK RELEASE UNIT (30 kn)
HIGH LOAD LOW SHOCK RELEASE UNIT (30 kn) Jens Müller (1), Christian Anderau (2) (1) Astrium GmbH, 81663 München (Germany), Email: Jens.mueller@astrium.eads.net (2) RUAG Aerospace AG, Widenholzstr. 1, 8304
More informationEPSILON 7 MOTOR. User manual supplement Edition 2 / 11_2013
EPSILON 7 MOTOR User manual supplement Edition 2 / 11_2013 English The EPSILON 7 Paramotor In this supplement to the ADVANCE EPSILON 7 manual you will find everything you need to know for flying this
More informationAirworthiness Directive
Airworthiness Directive AD No.: 2019-0018 Issued: 30 January 2019 Note: This Airworthiness Directive (AD) is issued by EASA, acting in accordance with Regulation (EU) 2018/1139 on behalf of the European
More informationAnti-Surge Thick Film Chip Resistors
FEATURES EXCELLENT ANTI-SURGE & ANTI-SULFUR CHARACTERISTICS AEC-Q200 QUALIFIED RATED POWER UPGRADE IN SMALLER PACKAGE SIZE AVAILABLE IN ± TOLERANCE BOTH FLOW SOLDER AND REFLOW SOLDERING ARE APPLICABLE
More informationHow it works. Rigging: Take off: Flying: Landing: Warranty:
How it works The Mosquito harness is a separate unit that allows a normal hang glider to become a foot-launched powered aircraft. Whilst on the ground 2 legs extend below the engine, keeping the propeller
More informationSpecial Condition C-04 on Interaction of Systems and Structure on helicopters configured with Fly-by-Wire (FBW) Flight Control System (FCS)
Special Condition C-04 on Interaction of Systems and Structure on helicopters configured with Fly-by-Wire (FBW) Flight Control System (FCS) This Special Condition is published for public consultation in
More informationNotification of a Proposal to issue an Airworthiness Directive
Notification of a Proposal to issue an Airworthiness Directive PAD No.: 18-143 Issued: 24 October 2018 Note: This Proposed Airworthiness Directive (PAD) is issued by EASA, acting in accordance with Regulation
More informationMODULE 11 CPS in Other Vehicles
Topic National Child Passenger Safety Certification Training Program MODULE 11 CPS in Other Vehicles Module Agenda: 15 Minutes Suggested Timing 1. Introduction 2 2. Appropriate Car Seats and Booster Seats
More informationISO INTERNATIONAL STANDARD. Road vehicles Roof load carriers Part 4: Magnetic fixing devices
INTERNATIONAL STANDARD ISO 11154-4 First edition 2004-10-15 Road vehicles Roof load carriers Part 4: Magnetic fixing devices Véhicules routiers Dispositifs porte-charges de toit Partie 4: Dispositifs à
More informationE/ECE/324/Rev.2/Add.128/Rev.1/Amend.2 E/ECE/TRANS/505/Rev.2/Add.128/Rev.1/Amend.2
E/ECE/324/Rev.2/Add.128/Rev.1/Amend.2 26 July 2017 Agreement Concerning the Adoption of Uniform Technical Prescriptions for Wheeled Vehicles, Equipment and Parts which can be Fitted and/or be Used on Wheeled
More informationContact person Date Reference Page Michael Lindblad F013838C 1 (1) Sustainable Built Environment
issued by an Accredited Testing Laboratory Contact person Michael Lindblad 2015-09-17 5F013838C 1 (1) Sustainable Built Environment +46 10 516 58 58 Michael.Lindblad@sp.se 1002 ISO/IEC 17025 Johanson Design
More information1. Semi- and centre-axle trailers To enable the automatic load sensing function to operate, it is necessary to define certain parameters as follows:
Commercial Vehicle Systems Product DATA Function Load Sensing Function (pneumatic suspension) PD-4-F00 The Load Sensing Function (LSF) of the TEBS Brake Module is used to replace the function of a load
More informationSAFETY COMPLIANCE TESTING FOR FMVSS NO. 214S SIDE IMPACT PROTECTION (STATIC)
REPORT NUMBER 214-GTL-09-002 SAFETY COMPLIANCE TESTING FOR S SIDE IMPACT PROTECTION (STATIC) MAZDA MOTOR CORPORATION 2009 MAZDA 3, PASSENGER CAR NHTSA NO. C95400 GENERAL TESTING LABORATORIES, INC. 1623
More informationNOTIFICATION
14401 Keil Road NE, Aurora, Oregon, USA 97002 PHONE 503-678-6545 FAX 503-678-6560 www.vansaircraft.com info@vansaircraft.com Service Letters and Bulletins: www.vansaircraft.com/public/service.htm NOTIFICATION
More informationE/ECE/324/Rev.1/Add.50/Rev.3/Amend.2 E/ECE/TRANS/505/Rev.1/Add.50/Rev.3/Amend.2
26 April 2018 Agreement Concerning the Adoption of Harmonized Technical United Nations Regulations for Wheeled Vehicles, Equipment and Parts which can be Fitted and/or be Used on Wheeled Vehicles and the
More information2000 BUICK LESABRE A 3.8 V6 (K) GAS Excellent
2000 BUICK LESABRE A 3.8 V6 (K) GAS Excellent Report Summary Report Name VehicleMRI Complete+ Report Number 606 Report Time 03/15/2012 3:22 PM Performed By Erik Horn Company ID 55 Vehicle Information VIN
More informationAgilent 1290 Infinity Autosampler
Agilent 1290 Infinity Autosampler Installation of the Large Volume Injection Kit General Information This note describes how to install the large volume injection kit into an Agilent 1290 Infinity Autosampler.
More informationTEST REPORT IEC Information technology equipment Safety Part 1: General requirements
Test Report issued under the responsibility of: TEST REPORT IEC 60950-1 Information technology equipment Safety Part 1: General requirements Report Number.... : 221868-CI3-2 CB DE1-56824 Date of issue...
More informationTYPE-CERTIFICATE DATA SHEET
TYPE-CERTIFICATE DATA SHEET No. E. 075 for ASTAZOU XIV series engines Type Certificate Holder 64510 Bordes France For Models: ASTAZOU XIV B ASTAZOU XIV H TE.CERT.00052-001 European Aviation Safety Agency,
More information