<?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%">Heer, R</style></author></authors></contributors><titles><title><style face="normal" font="default" size="100%">203. A Simple Method for Determination of the Maximum Payload</style></title><secondary-title><style face="normal" font="default" size="100%">17th Annual Conference, Belmont Plaza Hotel, New York, New York, May 19-22</style></secondary-title></titles><keywords><keyword><style  face="normal" font="default" size="100%">02. Aircraft Loading - Payload</style></keyword></keywords><dates><year><style  face="normal" font="default" size="100%">1958</style></year><pub-dates><date><style  face="normal" font="default" size="100%">5/19/58</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=41116</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%">New York, New York</style></pub-location><pages><style face="normal" font="default" size="100%">7</style></pages><language><style face="normal" font="default" size="100%">eng</style></language><abstract><style face="normal" font="default" size="100%">This paper was presented at the Airline Session, Seventeenth National Conference of the S.A.W.E. May 19-22, 1958, Belmont Plaza Hotel, New York, New York.
The method of Payload Computation described herein enables us to determine the max. allowable Payload based on fuel (Total fuel and Trip fuel) and the know Gross Weight Limits. The application of this system eliminates the various calculations which were necessary on the Loadsheet till now. The computer offers further the advantages to decide the max. Total Fuel, if the actual Payload and Trip fuel are given. The Payloads mentioned on the computer are based on a Standard Operating Weight Empty composed of a Fleet Basic Weight, Standard Pantry and Crew Weights.
This paper goes over the variables and provides some examples from the Payload Computer. After a short time of training it is possible to use the Computer very simply and thus eliminate considerable work and with a system which is practically foolproof. The present model serves only to illustrate the method. 
</style></abstract><work-type><style face="normal" font="default" size="100%">2. AIRCRAFT LOADING - PAYLOAD</style></work-type><accession-num><style face="normal" font="default" size="100%">0203</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>