Accession Number:

AD0249771

Title:

STRUCTURAL TEST PROGRAM F-106A AIRPLANE

Descriptive Note:

Corporate Author:

WRIGHT AIR DEVELOPMENT DIV WRIGHT-PATTERSON AFB OH ENGINEERING TEST DIV

Report Date:

1960-08-01

Pagination or Media Count:

72.0

Abstract:

The F-106 airplane was subjected to a complete static test program covering all of the critical flight, landing and ground handling conditions.

Subject Categories:

  • Attack and Fighter Aircraft

Distribution Statement:

APPROVED FOR PUBLIC RELEASE