Model: 4068224-800

Turbine Engine Afterburner

Properties:

End Application
Aircraft eng 100-pw-220
Criticality Code Justification
Agav
Engine Section Location
Afterburner
NSN
2840-01-344-3238
Part Number
4068224-800
Description
Afterburner,turbine Engine
CAGE

A chamber in which additional fuel is injected into, the exhaust gases, and reheating the gases to develop increased thrust. It consists of combustion area, flame holders, injection nozzles and an exhaust ejector.

Part 4068224-800 NSN 2840-01-344-3238

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
60031
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:
U
ESD:
ESD:
MMAC:
CRITL:
Y

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
114030
UFC:
64100
LTL:
200.0
LCL:
--
WCC:
593
TCC:
2
SHC:
R
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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