Model: 5103T24G02

Turbine Engine Afterburner Liner

Properties:

End Application
Preprovisioning support navicp is poe
NSN
2840-01-443-4130
Part Number
5103T24G02
Description
Liner,afterburner,turbine Engine
CAGE
99207

A cylindrical shaped item positioned inside the afterburner, turbine engine.It is designed to direct the flow of hot gases to the exhaust ejector and to protect the afterburner against thermal shocks.

Part 5103T24G02 NSN 2840-01-443-4130

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
52351
FIIG:
A530F0
Concept No.:
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:
A
ESD:
ESD:
MMAC:
CRITL:
X

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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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