Model: 4070852-01

Aircraft Gas Tur Compressor Vane

Special Features:

T.O. 2j-f100-54

Properties:

Overall Length
6.400 inches
End Application
F100pw0229 aircraft engine
Design Type
Axial compressor
Blade Attachment Method
Lock
Criticality Code Justification
Agav
Engine Section Location
Compressor
Stage Number
2
Material
Titanium alloy vane
Material Specification
Ams4928 assn standard single material response vane
NSN
2840-01-321-0702
Part Number
4070852-01
Description
Vane,compressor,aircraft Gas Tur
CAGE
77445

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 4070852-01 NSN 2840-01-321-0702

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:
NZ
CRITL:
F

Freight Classification

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