Turbibe e exhaust nozzle control (NSN 2995-01-091-1441)
End Application
J79-ge-15/15a/15b aircraft engine
Reference Data And Literature
T.O.6j3-8-7-4, f.2; nozzle area control; t.O.2j-j79-44, f.47
General Description
Dist between support arms 5.824 in.Max, dist ctr bore of side arm to ctr of throttle shaft 8.776 in.Max, dist ctr feedback shaft to ctr elec receptacle 4.60 in.Nom
Fsc Application Data
Aircraft eng fuel system components
Reference Number Differentiating Characteristics
As differentiated by source control no. 512d715p17
