INSTALLED SYSTEMS FUNCTIONAL TESTS REPORT

Abstract

The installed systems tests demonstrate that the aircraft systems function in accordance with design requirements. Tests were divided into thirteen major functional areas as follows: Electrical system checkout; surface gains and hysteresis; flight controls stability; flight mode conversion sequence; cockpit checkout; engine run temperature survey; engine run electrical system checkout; auto-stability tests; fan flight trim rates; landing gear tests; controls proof loads; weight-balance and fuel tests; fire extinguisher system tests.

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Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1964
Accession Number
AD0657996

Entities

Organizations

  • General Electric

Tags

Communities of Interest

  • Air Platforms
  • Weapons Technologies

DTIC Thesaurus Topics

  • Aerodynamic Configurations
  • Aircraft Equipment
  • Aircrafts
  • Attitude Indicators
  • Control Panels
  • Control Systems
  • Control Systems Engineering
  • Fire Extinguishers
  • Fuselages
  • Landing Gear Doors
  • Measurement
  • Nose Wheels
  • Spars
  • Stabilization Systems
  • Telemetry Equipment
  • Test Equipment
  • Trim Tabs

Readers

  • Aerospace Test and Evaluation
  • Aviation Science / Aeronautics.
  • Internal Combustion Engine (ICE) Technology.