Main fuel control, p/n 8062-459, for f108 aircraft eng
General Description
Cres per ams5350, hardened 32-45 rc; clevis one end 0.158 - 0.162 in. W; mtg holes at end of right-angled link 2.00 in. L c-to-c, leg 0.87 in. L outside edge to mtg hole cen; part of linkage assembly 5362-228