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)
Supersonic Transport Development Program. Phase III Proposal. Boeing Model 2707. Flight Controls and Hydraulics Subsystem Specification
1966
143 pages
Report
No indication
English
Aircraft , Hydraulic & Pneumatic Equipment , Flight control systems , Supersonic aircraft , Hydraulic equipment , Jet transport planes , Specifications , Design , Cost effectiveness , Operation , Reliability , Maintenance , Life expectancy , Angle of attack , Attitude indicators , Warning systems , Automatic pilots , Servomechanisms , Diagrams , Mechanical drawings , Stabilization , Electronic equipment , Roll , Pitch(Motion) , Yaw , Computer programming , Ailerons , Elevons , Management planning and control , Flight testing , Boeing 2707 aircraft , Supersonic transports