T-46A Flight Test Reports Jan - Mar 87

reportActive / Technical Report | Accesssion Number: AD1183314 | Open PDF

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.

Author(s):
Geiger, Jeannine
Author Organization(s):
Air Force Test Center
Funding Organization(s):
Air Force Test Center, Edwards , CA
Document Type:
Technical Report/Other
Publication Date:
2022 Oct 25
Pagination:
98

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution Code:
A - Approved For Public Release
Distribution Statement: Public Release

RECORD

Collection: TRECMS
Identifying Numbers
Project Number(s):
G0959
Subject Terms
Communities of Interest:
No COI(s) Identified
Keyword(s):
T-46A aircraft
Creation Date:
2022 Oct 26
Update Date:
2023 Feb 07