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Design Objectives for Handling Qualities of Transport Aircraft
- Aerospace Standard
Published July 11, 2007 by SAE International in United States
Downloadable datasets availableAnnotation ability available
This document specifies the requirements for the design objectives for handling qualities applicable to transport aircraft operating in the subsonic, transonic, and supersonic speed range. These objectives are not necessarily applicable to rotor or VTOL aircraft.
This document has been reaffirmed to comply with the SAE 5-Year Review policy.
|Aerospace Standard||Flight Envelope Awareness/Protection|
|Aerospace Standard||Design Objectives For Handling Qualities Of Transport Aircraft|
|Book||Flight Dynamics Principles, 3rd Edition|
Data Sets - Support Documents
|Unnamed Dataset 1|
The SAE S-7 Committee was formed to fulfill a need for the air transport industry to monitor itself with respect to uniformity of cockpit design for air transport aircraft.Standardization of the flight deck is becoming increasingly important to both operators and manufacturers. The objective is to design for the operational efficiencies necessary to maintain a competitive and viable air transportation industry. This must be accomplished while maintaining or improving the existing levels of operating efficiencies and safety. The S-7 Committees is committed to serving this purpose. This is an international committee of members representing major aircraft manufacturers, airlines from United States, Europe, and the Far East, as well as equipment designers, manufacturers, regulatory authorities, and other interested parties.
|N69-22539||This document is not part of the subscrption.|
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