Commercial Supersonic Transport Program. Phase II-C. Interim Aircraft Performance Assessment Report. Flight Instrumentation Performance Specification
Commercial Supersonic Transport Program. Phase II-C. Interim Aircraft Performance Assessment Report. Flight Instrumentation Performance Specification
This specification establishes the design, construction, performance requirements, and test objectives of the flight instrumentation equipment for the Model 733 supersonic transport. This specification covers the following flight instrumentation equipment: Attitude director indicator; Horizontal situation indicator; Flight director computer; Comparator warning and approach gate monitor; Approach progress annunciator; Radio magnetic indicator; Standby attitude/heading indicator; Radio altimeter; and Radar altitude/vertical speed indicator. System performance requirements established herein are design objectives to be applied to the prototype airplanes. Application of these requirements to production airplane design will be established after prototype flight testing. (Author)
Document information
Commercial Supersonic Transport Program. Phase II-C. Interim Aircraft Performance Assessment Report. Flight Instrumentation Performance Specification
1965
33 pages
Report
No indication
English
Aircraft , Avionics , Jet transport planes , Flight control systems , Flight instruments , Supersonic aircraft , Flight testing , Attitude control systems , Performance(Engineering) , Stall warning indicators , Radio altimeters , Airspeed indicators , Attitude indicators , Ground position indicators , Course indicators , Rate of climb indicators , Rate of descent indicators , Quality control , Specifications , Altimeters , Flight director computers , Supersonic transports