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Accession Number:
AD0804705
Title:
SUPERSONIC TRANSPORT DEVELOPMENT PROGRAM. PHASE III PROPOSAL. BOEING MODEL 2707. FLIGHT CONTROLS AND HYDRAULICS SUBSYSTEM SPECIFICATION,
Corporate Author:
BOEING CO SEATTLE WA SUPERSONIC TRANSPORT DIV
Report Date:
1966-09-06
Abstract:
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
Pages:
0143
Contract Number:
FA-SS-66-5
File Size:
0.00MB
