<?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%">Walters, C S</style></author></authors></contributors><titles><title><style face="normal" font="default" size="100%">1075. Digital Computer Applications to Weight and Balance Analysis</style></title><secondary-title><style face="normal" font="default" size="100%">34th Annual Conference, Seattle, Washington, May 5-7</style></secondary-title></titles><keywords><keyword><style  face="normal" font="default" size="100%">12. Weight Engineering - Computer Applications</style></keyword></keywords><dates><year><style  face="normal" font="default" size="100%">1975</style></year><pub-dates><date><style  face="normal" font="default" size="100%">5/5/75</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=40526</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%">Seattle, Washington</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%">Aviation Technology Incorporated computer products described herein provide a more rapid,  positive sequence, 
precise computation of critical preflight and flight operating data for aircraft than is presently available. 
Although computation requirements discussed are applicable to all aircraft, the necessity for precise computation 
is critical for high performance heavy aircraft and in particular, transport/cargo carriers which operate under a 
multitude of load  variations and are subject to many restrictive flight operational parameters. 
By use of microprogramming and application of modern  technology in micro-circuitry the product result is a digital, 
sequenced controlled and programmed computer dedicated to the solution of aircraft  weight and balance and inflight engineering calculations.</style></abstract><work-type><style face="normal" font="default" size="100%">12. WEIGHT ENGINEERING - COMPUTER APPLICATIONS</style></work-type><accession-num><style face="normal" font="default" size="100%">1075</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></record></records></xml>