Model: 634E608P20

Aircraft Gas Tur Compressor Vane

Properties:

Overall Length
Between 4.061 inches and 4.065 inches
Overall Width
Between 1.260 inches and 1.275 inches
Material Thickness
Between 0.0193 inches and 0.0207 inches
Design Type
Compressor
Blade Attachment Method
Slot
Part Name Assigned By Controlling Agency
Vane, turbine engine
Engine Section Location
Compressor
Stage Number
88
Material
Steel
Material Specification
B50t1132, b5051137, cagec 99207 mfr ref single material response
NSN
2840-00-711-5742
Part Number
634E608P20
Description
Vane,compressor,aircraft Gas Tur
CAGE
24446

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 634E608P20 NSN 2840-00-711-5742

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:
X

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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