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Aircraft Gas Tur Compressor Vane

Model / MPN: 702051CL5 | NSN: 2840-00-076-9779
ITAR Registered seal

A component of a vane assembly, compressor, aircraft gas turbine engine. It is designed to receive air from the preceding compressor blades and deliver it to the succeeding row of compressor blades, diffuser, or combustion area at correct pressure, velocity and direction.

Product Details
NATO Stock Number
2840-00-076-9779
Sold in multiples of
DEMIL
DEMIL/MLI
Overall Length
Between 2.614 inches and 2.663 inches
Overall Width
Between 1.104 inches and 1.124 inches
End Application
J60 aircraft engine
Blade Attachment Method
Pin
Criticality Code Justification
Agav
Engine Section Location
Combustion chamber
Stage Number
1
Material
Steel vane
Material Specification
Ams5385 assn standard single material response vane
702051CL Series Parts

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702051CL5 Cross Reference