Model: 506959

Aircraft Gas Combustion Chamber
Description:

16.135 inches overall length, acft engine j60 end item identification, agav criticality code justification, combustion chamber engine section location.

Properties:

Overall Length
16.135 inches
End Application
Aircraft engine j60
Criticality Code Justification
Agav
Engine Section Location
Combustion chamber
Material
Steel
Material Specification
Hastelloy x assn standard single material response
NSN
2840-00-015-1682
Part Number
506959
Description
Chamber,combustion,aircraft Gas
CAGE
77445

The portion of an engine, gas turbine, aircraft in which fuel is burned. it may be an annular type in which the space between the circular inner and outer cylinders form the burning chamber or it may be the multi-arrangement can type in which separate can like burn cylinders are positioned in a circular arrangement within an inner and outer case.

Part 506959 NSN 2840-00-015-1682

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
50337
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

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
8.0 X 8.0 X 18.0
Paclk Weight:
4.5000lbs
Item Weight:
0.0000lbs
Item Dim:
--
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
P
SPI No.:
F007984061
SPI Rev.:
SPC Mkg:
ZZ
LVL_A:
LVL_B:

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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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