FAA Research, Development, and Airworthiness Compliance for General Aviation Aircraft

660217

01/01/1966

Event
2nd Annual Business Aircraft Conference
Authors Abstract
Content
Aeronautical safety research and development work can provide a substantial contribution to the improvement in airworthiness standards and safety. Six representative Federal Aviation Agency research and development projects are described and the procedures employed to establish and conduct the work are outlined. The six projects deal with airframe strength, exhaust and heater systems, stability augmentation systems, a study of design features which may induce pilot error, new display and control configurations, and means of eliminating asymmetric thrust in light twin-engine airplanes.
The functions of the Federal Aviation Agency Engineering and Manufacturing Division in the development and application of airworthiness standards to type certification are discussed. Four current projects involving the development of standards for General Aviation aircraft, are considered. They are Oxygen Equipment and Supply, Minimum Performance Standards for Radio Navigation & Communications Equipment, Ice Protection Requirements, and Maximum Operating Altitude.
Meta TagsDetails
DOI
https://doi.org/10.4271/660217
Pages
12
Citation
Weeks, W., and Hoekstra, H., "FAA Research, Development, and Airworthiness Compliance for General Aviation Aircraft," SAE Technical Paper 660217, 1966, https://doi.org/10.4271/660217.
Additional Details
Publisher
Published
Jan 1, 1966
Product Code
660217
Content Type
Technical Paper
Language
English