Model: 9685M13P21
Aircraft Gas Tur Compressor Vane1.345 inches overall length, 0.935 inches overall width, acft eng tf-39 end item identification, axial compressor design type, agav criticality code justification.
Special Features:
63 aa microinch surface finish
Properties:
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.
Part 9685M13P21 NSN 2840-00-001-2114
Material Classification
Hazardous material, precious metals, criticality, enviroment, and electrostatic discharge indicatorsPackaging & Shipping
Freight Classification
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Schedule B and Export
- Schedule B: 8411997050
- SITC: 71499
- End Use: Engines and turbines for military aircraft
- NAICS: 336412
- USDA: 1
Freight Class: Parts of gas turbine aircraft engines, other than for use in civil aircraft
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