This content is not included in your SAE MOBILUS subscription, or you are not logged in.
Design Objectives For Handling Qualities Of Transport Aircraft
- Aerospace Standard
Published February 01, 1994 by SAE International in United States
This recommended practice sets forth 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.
Data Sets - Support Documents
No Datasets Available
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.
* Redlines comparisons are available for those standards listed in the Revision History that contain a radio button. A redline comparison of the current version against a revision is accomplished by selecting the radio button next to the standard and then selecting 'compare'. At this time, Redline versions only exist for some AMS standards. SAE will continue to add redline versioning with ongoing updates to SAE MOBILUS.