Model: 555211

Aircraft Combustion Chamber Case

Special Features:

Original name case, centrifugal compressor, turbine engine

Properties:

Overall Length
Between 6.353 inches and 6.413 inches
Diameter
Between 38.438 inches and 38.442 inches
End Application
Aircraft eng j57
Design Type
Centrifugal
Hardness Rating
25.0 rockwell c outer case and 33.0 rockwell c outer case
Engine Section Location
Compressor
Precious Material
Silver
NSN
2840-00-185-3554
Part Number
555211
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 555211 NSN 2840-00-185-3554

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:
S
ESD:
ESD:
MMAC:
CRITL:
X

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
--
Paclk Weight:
9,999.9000lbs
Item Weight:
--
Item Dim:
--
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
A
SPI No.:
F004083680
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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