INSTALLED SYSTEMS FUNCTIONAL TEST PROCEDURE.

Abstract

The purpose of these tests is to demonstrate that the XV-5A aircraft systems function in accordance with the design requirements. The testing procedure is divided into 12 major tests. The order of appearance is the desired chronological order. When the aircraft is received for functional tests, the hydraulic and pneumatic systems will have been flushed, filled and bled in accordance with Ryan Report 14359-6. The controls will have been rigged in accordance with Ryan Report 14395-5. (Author)

Document Details

Document Type
Technical Report
Publication Date
Nov 01, 1963
Accession Number
AD0657991

Entities

Organizations

  • General Electric

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aerospace Craft
  • Aerospaceplanes
  • Aircrafts
  • Fans
  • Lift Fans
  • Research Aircraft
  • Space Systems
  • Vehicles

Readers

  • Aerospace Test and Evaluation
  • Military History of the United States in the 20th Century.