Model: 521208

Aircraft Combustion Chamber Case

Properties:

Overall Length
Between 0.045 inches and 0.055 inches
Diameter
Between 1.690 inches and 1.710 inches
End Application
Aircraft eng tf33
Criticality Code Justification
Agav
Engine Section Location
Combustion chamber
Material
Steel
NSN
2840-01-160-1135
Part Number
521208
Description
Case,combustion Chamber,aircraft
CAGE
77445

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 521208 NSN 2840-01-160-1135

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:
RV
CRITL:
Y

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
133300
UFC:
63220
LTL:
RATING VARIABLE
LCL:
--
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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