Model: 6009T99G01

Aircraft Combustion Chamber Case

Properties:

Overall Length
10.000 inches
Diameter
16.926 inches
End Application
J-85 aircraft engine
Hardness Rating
23.0 rockwell c outer case
Criticality Code Justification
Agav
Engine Section Location
Combustion chamber
Material
Steel outer case
Material Specification
B50t73a mfr ref single material response outer case
NSN
2840-00-832-3326
Part Number
6009T99G01
Description
Case,combustion Chamber,aircraft
CAGE
99207

A case that is an integral part of an engine, gas turbine, aircraft, designed to surround and protect a chamber, combustion, aircraft gas turbine engine.

Part 6009T99G01 NSN 2840-00-832-3326

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
50545
FIIG:
A10700
Concept No.:
3
App. Key:
D
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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