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430. Airport Analysis and the Development of Turbine Operating Weights at United Air Lines
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Title | 430. Airport Analysis and the Development of Turbine Operating Weights at United Air Lines |
Publication Type | Conference Paper |
Paper Number | 0430 |
Year of Publication | 1964 |
Authors | Cooke, C. M. |
Paper Category | 1. AIRCRAFT LOADING - GENERAL |
Conference | 23rd National Conference / Sheraton, Dallas Hotel, Southland Center, Dallas, Texas May 18-21 |
Conference Location | Dallas, Texas |
Publisher | Society of Allied Weight Engineers, Inc. |
Date Published | 5/18/64 |
Abstract | The purpose of this paper is to outline for the members of the Society of Weight Engineers the United Air Lines approach to: The following methods of airport analysis and gross weight calculations are being used at United’s San Francisco Flight Engineering Division. O u r system was designed at the start of jet service in 1959 to show compliance with FAA's Special Regulation SR-4228. Steady improvement of our methods has been due largely to experience gained. Turbine take-off weights were originally computed using fight path overlays over runway and obstacle profiles. This method, while adequate for piston take-off weights, proved inadequate for jets. Since 100% temperature accountability is required for turbine take-off weights, an easier method of computation became necessary. The usually tedious job of preparing airplane operating weights is a result of a specific Federal requirement. This requirement states t h a t 9n analysis of each airport runway must be made whenever operations at that airport are planned. CAR 40-519 para. 8, requires take-off, en route and landing weight limitations to be part of a manual for "Guidance of Flight and Ground Personnel." The United Air Lines airplane Flight Manuals prepared for each airplane type, i e : E-8, B-720, 727 and Caravelle, contain a chapter for operating weights. |
Pages | 28 |
Key Words | 01. Aircraft Loading - General |
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