Accession Number:

ADA031110

Title:

Product-Improvement Test of OH-6A Rotor Blades with Increased Twist and Contour Tolerances.

Descriptive Note:

Final rept.

Corporate Author:

ARMY AVIATION TEST BOARD FORT RUCKER ALA

Personal Author(s):

Report Date:

1968-12-04

Pagination or Media Count:

17.0

Abstract:

The aircraft manufacturer, working with the LOH Project Manager, presented an Engineering Change Proposal to increase the parameters of the main-rotor blade tolerances for OH-6A helicopters. On 12 August 1968 the US Army Test and Evaluation Command directed the US Army Aviation Test Board USAAVNTBD to conduct a product-improvement test of OH-6A rotor blades with increased twist and contour thickness tolerances.

Subject Categories:

  • Helicopters

Distribution Statement:

APPROVED FOR PUBLIC RELEASE