T-46A Flight Test Reports Jan - Mar 87

Abstract

Air abort due to instrumentation parameter 742 inoperative. No flight test data obtained. On the ground, gusty wind conditions caused fluctuations in the H1 engine (RPM, EGT, fuel flow) which were elimated by selecting manual fuel control. The #2 engine, which has the 110D record 6 ECU, operated normally.

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Document Details

Document Type
Technical Report
Publication Date
Oct 25, 2022
Accession Number
AD1183314

Entities

People

  • Jeannine Geiger

Organizations

  • Air Force Test Center

Tags

DTIC Thesaurus Topics

  • Air Force
  • Aircrafts
  • Airframes
  • Altitude
  • Control Systems
  • Data Analysis
  • Flight
  • Flight Instruments
  • Frequency
  • Fuel Pumps
  • Indicators
  • Landing Gear
  • Mach Number
  • Nose Wheels
  • Test And Evaluation
  • Trim Tabs
  • Warning Systems

Readers

  • Aerospace Engineering
  • Astronomy and Astrophysics.
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