Inconel 625 ams5599; 29.900 in.Lg, 26.280 in.Dia o/a; 30 holes 0.221 in.Dia on a 25.860 in.Dia bolt circle;
A single stationary item designed for the purpose of directing air at the proper angle and velocity to a rotor, turbine, aircraft gas turbine engine. it has provisions for attaching to a case (3), turbine, aircraft gas turbine engine. it may have an inner support shroud.
Classification: Parts of gas turbine aircraft engines, other than for use in civil aircraft
NSN 5835-01-388-5198
NSN 6650-00-253-9195
NSN 5895-01-490-6314
NSN 5965-00-289-6280
NSN 6130-01-275-2174
NSN 5960-00-628-2003
NSN 5998-01-282-9748
NSN 5965-01-641-3291
NSN 5925-00-451-2061
NSN 5960-01-328-8248
NSN 5835-01-009-2417
NSN 5945-01-537-2486