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03079aam a22004454a 4500 001 03B7A634FE5F11E2B6A414D3DAD10320 003 SILO 005 20130806010419 006 m d f 007 cr cn||||||||| 008 041201s2004 dcua sb f000 0 eng 035 $a (OCoLC)70713400 040 $a NLM $c NLM $d GPO $d MvI $d SILO 042 $a pcc 060 10 $a WL 354 074 $a 0431-E-04 (online) 086 0 $a TD 4.210:04/18 100 1 $a DeWeese, Rick. 245 10 $a Evaluation of a head injury criteria component test device $h [electronic resource] : $b final report / $c Richard L. DeWeese, David M. Moorcroft. 260 $a Washington, DC : $b U.S. Dept. of Transportation, Federal Aviation Administration, Office of Aerospace Medicine, $c [2004] 300 $a iii, 16 p. : $b digital, PDF file. 538 $a Mode of access: Internet from the FAA web site. Address as of 10/4/07: http://www.faa.gov/library/reports/medical/oamtechreports/2000s/media/0418.pdf ; current access available via PURL. 500 $a Title from title screen (viewed on July 14, 2006). 500 $a Paper version available through the National Technical Information Service. 500 $a "November 2004." 504 $a Includes bibliographical references. 520 3 $a Aircraft seats that are certified to meet the requirements of 14 CFR Parts 23.562, 25.562, 27.562 and 29.562 must protect the occupant from serious head injury as defined by the Head injury criterion (HIC). Currently this is demonstrated during a dynamic sled test that includes a 50% male-size test dummy, the seat, and any surrounding aircraft structure that could be impacted by the occupant's head. To reduce cost and expedite design and certification, a means of demonstrating compliance using a component-level test was desired. A project to develop a component test method was initiated by the FAA Technical Center's Materials and Structures Branch, under contract to the National Institute for Aviation Research (NIAR) at Wichita State University (WSU). This effort resulted in the development of the HIC Component Test Device (HCTD) as described in FAA report DOT/FAA/AR-02-99. The HCTD consisted of a test dummy head attached to a pivoted arm that is propelled in an arc by an air actuator. The device was transferred to CAMI in Dec. 2002 for evaluation and further development. 500 $a "DOT/FAA/AM-04/18." 536 $g AM-B-03-PRS 96 650 0 $a Airplanes $x Evaluation. $x Safety measures $x Evaluation. 650 0 $a Head $x Prevention. $x Prevention. 776 0 $a DeWeese, Richard L. $t Evaluation of a head injury criteria component test device $h 16 p. $w (OCoLC)57126533 700 1 $a Moorcroft, David M. 710 1 $a United States. $b Office of Aerospace Medicine. 710 1 $a United States. $b National Technical Information Service 710 2 $a Civil Aerospace Medical Institute 856 40 $u http://purl.access.gpo.gov/GPO/LPS86540 941 $a 1 952 $l USUX851 $d 20160824035056.0 956 $a http://locator.silo.lib.ia.us/search.cgi?index_0=id&term_0=03B7A634FE5F11E2B6A414D3DAD10320Initiate Another SILO Locator Search