Model: 6028T94G03

Aircraft Combustion Chamber Case

Special Features:

Includes 1-9 stages

Properties:

Overall Length
15.655 inches
Diameter
18.100 inches
Material Thickness
0.186 inches
End Application
J85-ge-21b aircraft engine
Design Type
Axial compressor
Hardness Rating
35.0 rockwell c outer case and 43.0 rockwell c outer case
Criticality Code Justification
Agav
Engine Section Location
Compressor
Material
Steel outer case
NSN
2840-01-315-5108
Part Number
6028T94G03
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 6028T94G03 NSN 2840-01-315-5108

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:
OK
CRITL:
F

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
24.3 X 24.3 X 20.5
Paclk Weight:
45.0000lbs
Item Weight:
40.0000lbs
Item Dim:
018101810157
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
O
SPI No.:
F000001D76
SPI Rev.:
SPC Mkg:
17
LVL_A:
LVL_B:

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
133300
UFC:
63220
LTL:
RATING VARIABLE
LCL:
92.5
WCC:
593
TCC:
Z
SHC:
Z
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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