Accession Number:

AD0762832

Title:

Fatigue Evaluation of Wing and Associated Structure on Small Airplanes.

Descriptive Note:

Final technical rept.

Corporate Author:

FEDERAL AVIATION ADMINISTRATION WASHINGTON D C FLIGHT STANDARDS SERVICE

Personal Author(s):

Report Date:

1973-05-01

Pagination or Media Count:

39.0

Abstract:

Methods for evaluating the wing and associated structure for fatigue under the safe life and fail safe concept are outlined. Detailed procedures and scatter factors are given for full scale fatigue test, component test and the analytical methods of substantiation. Loading spectra are given for the various types of aircraft and usage. Author

Subject Categories:

  • Aircraft

Distribution Statement:

APPROVED FOR PUBLIC RELEASE