Cres, ams5536 and cres, ems73657 fscm 73342, 27 vanes equally spaced, 1.737 in.Min, 1.739 in.Max o/a lg, 7.350 in.Nom od, 1.823 in.Min, 1.825 in. Inside diameter
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 5965-01-324-6583
NSN 5925-00-822-0261
NSN 5855-01-444-4859
NSN 5855-01-180-5369
NSN 5895-00-828-3994
NSN 5835-01-013-9321
NSN 5925-00-265-2275
NSN 6145-01-347-3336
NSN 5950-01-285-3404
NSN 6220-01-063-8238
NSN 5990-00-518-3195
NSN 7035-01-560-8371