Accession Number:

ADA009878

Title:

T-39 Landing Gear Design Evaluation and Fatigue Analysis. Phase II. Volume 1 of III,

Descriptive Note:

Corporate Author:

BENDIX CORP SOUTH BEND IND ENERGY CONTROLS DIV

Personal Author(s):

Report Date:

1975-02-28

Pagination or Media Count:

148.0

Abstract:

The purpose of this report is to accomplish a fatigue damage evaluation of the original and revised main and nose landing gears of the North American Rockwell T-39 aircraft. The fatigue loads spectrum utilized in this evaluation is developed by Bendix ECD from flight test data supplied by Hill Air Force Base.

Subject Categories:

  • Training Aircraft

Distribution Statement:

APPROVED FOR PUBLIC RELEASE