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SUPERSONIC TRANSPORT PROGRAM. PHASE II-C REPORT. FLIGHT CONTROLS AND HYDRAULICS SUBSYSTEM SPECIFICATION. SST BOEING MODEL 2707,
BOEING CO SEATTLE WA SUPERSONIC TRANSPORT DIV
This specification establishes the requirements for performance, design, test and qualification of the Flight Controls and Hydraulics Subsystem, as applied to the prototype preproduction airplanes. This subsystem shall provide control of the airplane in response to pilot or guidance-navigation system commands and furnish hydraulic power to the Landing Gear Subsystem, D6A10108-1. The subsystem shall consist of Primary Flight Controls, Secondary Flight Controls, Automatic Flight Controls and Hydraulic Power. Author
See also Rept. no. D6A10120-5, AD-805 683L.