Accession Number:
AD0739331
Title:
Arrested Landing Fatigue Test of Model C-2A Airplane.
Descriptive Note:
Final rept.,
Corporate Author:
NAVAL AIR DEVELOPMENT CENTER WARMINSTER PA
Personal Author(s):
Report Date:
1971-06-30
Pagination or Media Count:
39.0
Abstract:
A laboratory fatigue test was performed on a C-2A airframe to determine whether the airframe could sustain the effects of 3000 arrested landings. A total of 6000 arrested landing cycles were applied to the airframe during the test with no structural failures. With a test scatter factor of 2, the 600 test cycles are equivalent to 3000 service arrested landings. Author
Descriptors:
Subject Categories:
- Transport Aircraft