<?xml version="1.0" encoding="UTF-8"?><xml><records><record><source-app name="Biblio" version="6.x">Drupal-Biblio</source-app><ref-type>47</ref-type><contributors><authors><author><style face="normal" font="default" size="100%">Ursee, C R</style></author><author><style face="normal" font="default" size="100%">Wilbur, R L</style></author></authors></contributors><titles><title><style face="normal" font="default" size="100%">1669. Requirements for Second Generation Aircraft Weighing Systems</style></title><secondary-title><style face="normal" font="default" size="100%">44th Annual Conference, Arlington, Texas, May 20-22</style></secondary-title></titles><keywords><keyword><style  face="normal" font="default" size="100%">10. Weight Engineering - Aircraft Design</style></keyword></keywords><dates><year><style  face="normal" font="default" size="100%">1985</style></year><pub-dates><date><style  face="normal" font="default" size="100%">5/20/85</style></date></pub-dates></dates><urls><web-urls><url><style face="normal" font="default" size="100%">http://www.sawe.org/store/product_info.php?products_id=43814</style></url></web-urls></urls><publisher><style face="normal" font="default" size="100%">Society of Allied Weight Engineers, Inc.</style></publisher><pub-location><style face="normal" font="default" size="100%">Arlington, Texas</style></pub-location><pages><style face="normal" font="default" size="100%">6</style></pages><language><style face="normal" font="default" size="100%">eng</style></language><abstract><style face="normal" font="default" size="100%">Weighing of aircraft to determine weights, distribution and center of gravity is becoming more and more a critical and necessary operation. In order to achieve the desired goals, ten basic requirements have been set forth for the second generation of new weighing systems. These requirements involve accuracy, repeatability, linearity, simplicity, portability, ruggedness, size/weight, maintainability, calibration and temperature correction. These have been achieved in two prototype systems that have been in operation for the past five years.</style></abstract><work-type><style face="normal" font="default" size="100%">10. WEIGHT ENGINEERING - AIRCRAFT DESIGN</style></work-type><accession-num><style face="normal" font="default" size="100%">1669</style></accession-num><custom1><style face="normal" font="default" size="100%">Non-Member Price: $10.00. Members may download this paper for free. &lt;a href=&quot;http://www.sawe.org/dms&quot;&gt;Click here&lt;/a&gt;. (Login Required. See SAWE &lt;a href=&quot;http://www.sawe.org/faq&quot;&gt;Frequently Asked Questions&lt;/a&gt;.)</style></custom1><custom3><style face="normal" font="default" size="100%">10</style></custom3></record></records></xml>