Model: 124D275

Aircraft Gas Combustion Chamber

Properties:

Overall Length
Between 25.940 inches and 26.020 inches
End Application
Aircraft gas turbine and jet engines
Criticality Code Justification
Czbj
Engine Section Location
Combustion chamber
NSN
2840-00-313-4648
Part Number
124D275
Description
Chamber,combustion,aircraft Gas
CAGE
07482

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 124D275 NSN 2840-00-313-4648

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

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
133300
UFC:
63220
LTL:
RATING VARIABLE
LCL:
77.5
WCC:
593
TCC:
Z
SHC:
9
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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