Model: 21C6208G01

Aircraft Engine Machining Fixture

Special Features:

Steel

Properties:

End Application
J85-ge-21/-21a turbojet engine age.
Nominallength
14.000 inches
Nominalwidth
13.000 inches
Nominalheight
8.000 inches
Functional Description
Used during repair/maintenance of compressor rear spool
NSN
4920-01-089-9937
Part Number
21C6208G01
Description
Fixture,machining,aircraft Engine
CAGE
07482

A fixture designed to hold aircraft engine or auxiliary power unit individual parts, subassemblies, or assemblies in position for machining to design tolerances during modification or repair.

Part 21C6208G01 NSN 4920-01-089-9937

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
52377
FIIG:
A505C0
Concept No.:
1
App. Key:
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:
U
ESD:
ESD:
MMAC:
CRITL:
X

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
095190
UFC:
49790
LTL:
RATING VARIABLE
LCL:
70.0
WCC:
713
TCC:
Z
SHC:
Z
ACC:
Trailers/Vehicles

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Schedule B and Export
  • Schedule B: 8466208040
  • SITC: 73513
  • End Use: Industrial machines, other
  • NAICS: 333514
  • USDA: 1

Freight Class: Jigs and fixtures,nesoi,for machine tools

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