Download or read book Supersonic Transport Development Program Phase Iii Proposal Boeing Model 2707 Flight Deck Subsystem Specification written by George G. Burton and published by . This book was released on 1966 with total page 126 pages. Available in PDF, EPUB and Kindle. Book excerpt: This specification defines the objectives, criteria and configuration and establishes the requirements for performance, design, test, and qualification of the flight deck subsystem as applicable to the prototype supersonic transport airplane. Differences between the prototype and production airplanes are described in Supplement I. (Author).
Download or read book Supersonic Transport Development Program Phase Iii Boeing Model 2707 Flight Deck Subsystem Specification written by George G. Burton and published by . This book was released on 1966 with total page 163 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Supersonic Transport Development Program Phase Iii Proposal Boeing Model 2707 Air Induction Control Subsystem Specification written by BOEING CO SEATTLE WA SUPERSONIC TRANSPORT DIV. and published by . This book was released on 1966 with total page 139 pages. Available in PDF, EPUB and Kindle. Book excerpt: This specification defines objectives, criteria and configuration, and establishes requirements for performance, operation, design, test and qualification of the air induction control subsystem (hereinafter called the control subsystem) as applied to the prototype model supersonic transport airplane. Differences between the prototype and production airplanes are described in Supplement I. This subsystem is used to provide automatic and manual control of the air induction subsystem, (hereinafter called the inlet). There shall be one independent control subsystem for each of the four inlets. Each control subsystem changes the geometry of an inlet centerbody and operates its bypass louvers and takeoff doors to provide efficient inlet airflow diffusion and high performance inlet-engine airflow match. The subsystems include necessary hydraulic power generation, hydraulic power distribution equipment, and flight deck controls and displays. Power from the airplane electrical system and from each of the engines is required by the subsystem in order to accomplish its intended function. (Author).
Download or read book Supersonic Transport Development Program Phase Iii Proposal Boeing Model 2707 Flight Controls and Hydraulics Subsystem Specification written by E. See and published by . This book was released on 1966 with total page 143 pages. Available in PDF, EPUB and Kindle. Book excerpt: This specification defines the objectives, criteria, and configuration and establishes the requirements for performance, design, test, and qualification of the flight controls and hydraulic subsystem for the B-2707 supersonic transport airplane. Differences between the prototype and production airplanes are described in Supplement I. This subsystem shall provide control of the airplane in response to pilot or guidance-navigation commands and furnish hydraulic power to the landing gear subsystem. This subsystem shall consist of primary flight controls, secondary flight controls, automatic flight controls and hydraulic power. (Author).
Download or read book Supersonic Transport Development Program Phase Iii Proposal Boeing Model 2707 Fuel Subsystem Specification written by S. E. Lindstrom and published by . This book was released on 1966 with total page 47 pages. Available in PDF, EPUB and Kindle. Book excerpt: This specification defines the objectives, criteria, and configuration and establishes the requirements for performance, design, test, and qualification of the fuel subsystem for the prototype model supersonic transport airplane. This subsystem provides for the storage, distribution and management of fuel.
Download or read book Supersonic Transport Development Program Phase Iii Proposal Boeing Model 2707 Communications navigation Subsystem Specification written by Howard G. Barton and published by . This book was released on 1966 with total page 395 pages. Available in PDF, EPUB and Kindle. Book excerpt: This specification defines the objectives, criteria, and configuration, and establishes the requirements for performance, design, test, and qualification of the navigation and communication subsystem for the prototype model supersonic transport airplane. (Author).
Download or read book Supersonic Transport Development Program Phase Iii Proposal Boeing Model 2707 Environmental Control Subsystem Specification written by V. D. Warmbo and published by . This book was released on 1966 with total page 66 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Supersonic Transport Development Program Phase Iii Proposal Boeing Model 2707 B 2707 Model Specification written by R. G. Bush and published by . This book was released on 1966 with total page 309 pages. Available in PDF, EPUB and Kindle. Book excerpt: Contents: General Airplane Description; General Requirements; General Airplane Characteristics; Airframe Structures; Propulsion; Flight Deck Accommodations; Flight Controls; Hydraulic Power System; Electric Power System; Electronics; Passenger and Cargo Provisions; Environmental Control; Maintainability, and Standard Parts, Interchangeability, and Replaceability.
Download or read book Supersonic Transport Development Program Phase Iii Proposal Boeing Model 2707 Air Induction Subsystem Specification written by L. J. Kimer and published by . This book was released on 1966 with total page 94 pages. Available in PDF, EPUB and Kindle. Book excerpt: This specification defines the objectives, criteria, and configuration and establishes the requirements for performance, design, test, and qualification of the air induction subsystem for the prototype-model supersonic transport airplane. Differences between the prototype and production airplanes are described in Supplement I. The air induction subystem shall provide the engine with the quantity of air demanded at high-pressure recovery within the flow distortion limits of the engine. Four independent subsystems are required per airplane.
Download or read book Supersonic Transport Development Program Phase Iii Proposal Boeing Model 2707 Airframe Subsystem Specification written by John Katzinski and published by . This book was released on 1966 with total page 75 pages. Available in PDF, EPUB and Kindle. Book excerpt: This specification establishes the requirements for performance, design, test, and qualification for the Airframe Subsystem as applied to the prototype model supersonic transport airplenes. The airframe subsystem consists of the fuselage, empennage, wing and control surfaces. Discrete differences between the prototype model supersonic transport airplanes and production airplanes are included in Supplement I. (Author).
Download or read book Supersonic Transport Development Program Phase Iii Proposal Boeing Model 2707 Landing Gear Subsystem Specification written by T. A. Perara and published by . This book was released on 1966 with total page 53 pages. Available in PDF, EPUB and Kindle. Book excerpt: This specification defines the objectives, criteria, and configuration, and establishes the requirements for performance, design, test, and qualification of the Landing Gear Subsystem for the prototype model supersonic transport airplane. The subsystem defined herein consists of the landing gear structure, shock absorbers, wheels, brakes, tires, brake control, steering, extension and retraction, and position indication and warning.
Download or read book Supersonic Transport Development Program Phase Iii Boeing Model 2707 Starting Subsystem Specification written by Grant W. Ort and published by . This book was released on 1966 with total page 41 pages. Available in PDF, EPUB and Kindle. Book excerpt: This specification defines the objectives, criteria, and configuration, and establishes the requirements for performance, design, test and qualification of the starting subsystem (SS) for the prototype model supersonic transport airplane. Differences between the prototype and production airplanes are described in Supplement I. The SS provides for starting and windmill braking of the engine, drives the accessory drive subsystem (ADS) and its attached accessories in the engine disconnect mode, and supplies ground source or engine bleed air to the environmental control subsystem (ECS).
Download or read book Supersonic Transport Development Program Phase Iii Proposal Boeing Model 2707 Training Equipment Specifications written by Lewis H. Gray and published by . This book was released on 1966 with total page 29 pages. Available in PDF, EPUB and Kindle. Book excerpt: This specification establishes the performance, design, test, and qualification requirements for the flight simulator of Boeing Model 2707 production airplane (B-2707). The simulator will be used for training flight crews in both ground and flight operations.
Download or read book Supersonic Transport Development Program Phase Iii Proposal Boeing Model 2707 Technical Publications Specifications written by Lewis H. Gray and published by . This book was released on 1966 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Supersonic Transport Development Program Phase Iii Boeing Model 2707 Aircraft Integrated Data Subsystem Specification written by W. H. Burrell and published by . This book was released on 1966 with total page 33 pages. Available in PDF, EPUB and Kindle. Book excerpt: This specification defines the objectives, criteria and configuration and establishes the requirements for performance, design, test, and qualification of the Aircraft Integrated Data System (AIDS) for the prototype model supersonic transport airplane. The primary purpose of AIDS is to reduce maintenance cost and to improve aircraft availability and dispatch reliability. It accomplishes fault detection during flight and identifies aircraft system component failures. This information is presented as a readable output on board the airplane for use by the flight crew during flight and maintenance crew upon termination of the flight. The AIDS data may be further used to accomplish failure prediction by analyzing flight recorded system performance data with a ground based computer.
Download or read book Supersonic Transport Development Program Phase Iii Boeing Model 2707 Fuel Subsystem Specification written by S. E. Lindstrom and published by . This book was released on 1966 with total page 50 pages. Available in PDF, EPUB and Kindle. Book excerpt: This specification defines the objectives, criteria, and configuration and establishes the requirements for performance, design, test, and qualification of the fuel subsystem for the prototype model supersonic transport airplane. Differences between the prototype and production airplanes are described in Supplement I. This subsystem provides for the storage, distribution and management of fuel. (Author).
Download or read book Supersonic Transport Development Program Phase Iii Boeing Model 2707 Communications navigation radar Subsystem Specification written by Howard G. Barton and published by . This book was released on 1966 with total page 399 pages. Available in PDF, EPUB and Kindle. Book excerpt: This specification defines the objectives, criteria, and configuration, and establishes the requirements for performance, design, test, and qualification of the communications/navigation/radar subsystem for the prototype model supersonic transport airplane.
