Model: 6041T52G03

Turbine Afterburner Flameholder

Properties:

Overall Length
Between 7.290 inches and 7.350 inches
End Application
Aircraft eng j-85
Criticality Code Justification
Agav
Engine Section Location
Afterburner
Material
Steel
Material Specification
Ams 5537 assn standard single material response
NSN
2840-01-176-9140
Part Number
6041T52G03
Description
Flameholder,afterburner,turbine
CAGE
99207

An item designed to sustain flame and assist combustion stability in the conbustion section of a turbine engine afterburner by creating turbulence which provides even fuel and air mixture to assure continuous burnig.

Part 6041T52G03 NSN 2840-01-176-9140

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
61689
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:
Y

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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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