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 7035-01-132-7209
NSN 5895-01-130-1617
NSN 6135-01-435-6503
NSN 6240-01-557-0647
NSN 6145-00-946-2033
NSN 7035-00-922-5700
NSN 6105-01-331-6033
NSN 5985-00-518-3359
NSN 6645-01-561-7432
NSN 6610-00-121-4683
NSN 5910-01-607-0208
NSN 5910-00-153-4585