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Accession Number:
AD1183314
Title:
T-46A Flight Test Reports Jan - Mar 87
Report Date:
2022-10-25
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.
Document Type:
Conference:
Journal:
Pages:
98
File Size:
12.46MB
Contracts:
Grants:
Distribution Statement:
Approved For Public Release
