Accession Number:

AD0646282

Title:

MAIN LANDING GEAR DROP TEST REPORT

Descriptive Note:

Corporate Author:

GENERAL ELECTRIC CO CINCINNATI OH ADVANCED ENGINE AND TECHNOLOGY DEPT

Personal Author(s):

Report Date:

1964-03-01

Pagination or Media Count:

48.0

Abstract:

The shock absorber portion of the 1510L100 Main Landing Gear, but using a dummy cylinder, was tested on 2 August 1963, in accordance with the H. W. Loud Test Procedure 1510LTP-4, Revision A. The report presents the successful completion of the established test requirements.

Subject Categories:

  • VSTOL
  • Research and Experimental Aircraft

Distribution Statement:

APPROVED FOR PUBLIC RELEASE