Model: 6868825

Aircraft Gas Tur Compressor Vane

Special Features:

Original name vane, compressor stator, turbine engine

Properties:

Overall Length
8.980 inches
Material Thickness
Between 0.076 inches and 0.087 inches
End Application
Tf41 aircraft engine
Design Type
Compressor
Criticality Code Justification
Agav
Engine Section Location
Compressor
Material
Steel vane
Material Specification
Ams5504 assn standard single material response vane
NSN
2840-00-063-7248
Part Number
6868825
Description
Vane,compressor,aircraft Gas Tur
CAGE
73342

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 6868825 NSN 2840-00-063-7248

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
50611
FIIG:
A10700
Concept No.:
App. Key:
A
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

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
133300
UFC:
63220
LTL:
RATING VARIABLE
LCL:
--
WCC:
593
TCC:
Z
SHC:
9
ACC:
Equipment for Aircraft

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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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