Flow area 1.473 - 1.483.Pitch is 34deg 47min 28sec
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 5945-01-334-3886
NSN 6620-00-492-4936
NSN 6685-00-566-6783
NSN 6220-01-193-6542
NSN 6130-01-459-5528
NSN 5835-01-626-9603
NSN 5915-01-479-6403
NSN 4140-01-354-4404
NSN 5905-01-068-2955
NSN 6145-01-165-1436
NSN 5925-01-444-5274
NSN 6145-01-631-1788