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Contents: Policy with Regard to Control Techniques; Task Control; Schedule Planning and Control; Resource Planning and Control; and Management Review and Evaluation.
This document describes the Boeing Model 2707 Warranty Program that will be offered to airline customers for the United States Supersonic Transport (SST). During Phase II-C, Boeing solicited the airlines for their warranty recommendations. Airline suggesstions, coupled with Boeing's subsonic warranty experience and comprehensive analysis of supersonic warranty needs and the presently planned development program for the SST, provided the basis for the B-2707 Warranty Program set forth. This program will minimize financial risks associated with introducing the supersonic transport and will provide a further incentive for the manufacturer to design, develop, and build an airplane that is safe, reliable, and economically attractive.
This specification establishes the requirements for performance, design, test, and qualification of the Ground Support Equipment (GSE) required for the B-2707. Included are the general design requirements applicable to all GSE designed for the B-2702, a consolidated list of the GSE arranged by system requirements, and individual specification data for each item of equipment. This combined specification provides requirements planning information and technical data on all of the GSE presently identified. A prime consideration in GSE planning and definition has been to use existing inventory, existing standard, or modified standard GSE whenever possible. The extensive use of equipment in these categories for B-2707 support is indicated on the consolidated list. GSE identification is an output of the system engineering analysis process, which is continuously applied to define and verify the B-2707 support requirements. The specification will be refined and updated throughout the prototype development program to provide a current definition of the GSE requirements for effective and efficient air carrier ground operations.
This specification establishes the requirements for the performance and method of calculation for the B-2707 (PW) propulsion system. The Pratt + Whitney Aircraft JTF17A-21B engine performance data is the primary data for the production propulsion performance specification. Supplement 1 of this specification defines the prototype propulsion performance and method of calculation by showing the specific differences between the production and the prototype engines.
A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system and announced in Scientific and technical aerospace reports (STAR) and International aerospace abstracts (IAA).