Model: 108R857G51A

Aircraft Gas Tu Compressor Rotor

Special Features:

Original name compressor rotor, axial, turbine engine

Properties:

End Application
Aircraft engine j79-15/17
Design Type
Axial compressor
Criticality Code Justification
Agav
Engine Section Location
Compressor
NSN
2840-01-027-2425
Part Number
108R857G51A
Description
Rotor,compressor,aircraft Gas Tu
CAGE
07482

A single or multistage assembly designed to deliver air at the proper pressure, direction and velocity. it consists of disks, blades, hubs, and the like. it is the moving part of compressor, aircraft gas turbine engine. it has facilities for attaching to a shaft, turbine, aircraft gas turbine engine.

Part 108R857G51A NSN 2840-01-027-2425

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
50587
FIIG:
A10700
Concept No.:
App. Key:
J
Cond. Code:
1
Status:
A

Material Classification

Hazardous material, precious metals, criticality, enviroment, and electrostatic discharge indicators
HMIC
PMIC
ESD/EMI
ENAC
MMAC
CRITL
HMIC:
N
PMIC:
A
ESD:
ESD:
MMAC:
CRITL:
Y

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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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