Accession Number:

AD0827604

Title:

SUPERSONIC TRANSPORT DEVELOPMENT PROGRAM. PHASE 3. BOEING MODEL 2707. FLIGHT CONTROLS AND HYDRAULICS SUBSYSTEM SPECIFICATION

Descriptive Note:

Corporate Author:

BOEING CO SEATTLE WA SUPERSONIC TRANSPORT DIV

Personal Author(s):

Report Date:

1966-12-31

Pagination or Media Count:

153.0

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 prototype 2707-100 supersonic transport airplane. Differences between the prototype and production airplanes are described. 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.

Subject Categories:

  • Civilian Aircraft

Distribution Statement:

APPROVED FOR PUBLIC RELEASE