Accession Number:

AD0728009

Title:

Structural Integrity Investigation of Reworked S-2 Corrugated Wing Skin Panels.

Descriptive Note:

Final rept.,

Corporate Author:

NAVAL AIR DEVELOPMENT CENTER WARMINSTER PA AERO STRUCTURES DEPT

Personal Author(s):

Report Date:

1971-04-01

Pagination or Media Count:

38.0

Abstract:

Laboratory fatigue tests were performed on reworked S-2 corrugated wing skin panels to determine the effect on the structural integrity of skin material removal due to corrosion damage. Reworking of the S-2 aircraft corrugated wing skin panels, as performed by the Naval Air Rework Facilities, to remove corrosion damaged material, does not adversely affect the structural integrity of the panels. Author

Subject Categories:

  • Patrol and Reconnaissance Aircraft

Distribution Statement:

APPROVED FOR PUBLIC RELEASE