Contents: Configuration Design and Development -- Landing gear study, Body depth study, Vertical tail studies, Weight review, Interior arrangement development, and Landing gear deflection systems; Performance -- Wind tunnel testing, Performance analysis, Stability and control, Flight dynamics, Noise, and Airport compatibility; Structures -- Criteria and loads analysis, Stress analysis, Structural design, Flutter and dynamic loads analysis, Weight and balance analysis, and Structural and material tests; Propulsion -- Inlet and exhaust test and analysis, Engine performance analysis, Propulsion system integration, Fuel system, and Propulsion control; Systems -- Avionics, Flight controls, Hydraulics and electrical, Environmental control and oxygen systems, Fire detecting and extinguishing systems, Flight instrument systems, Accessory power drive system; and Design Support and Integration -- Maintainability engineering and Customer engineering.


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