Model: 6028T94G02

Aircraft Combustion Chamber Case

Special Features:

T.O. 2j-j85-94; includes stages 19; original name case, axial compressor, turbine engine

Properties:

Overall Length
15.600 inches
Diameter
Between 17.310 inches and 17.330 inches
End Application
Aircraft eng j85
Design Type
Axial compressor
Criticality Code Justification
Agav
Engine Section Location
Compressor
Material
Steel outer case
Material Specification
Ams5547 assn standard single material response outer case
NSN
2840-01-123-1050
Part Number
6028T94G02
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 6028T94G02 NSN 2840-01-123-1050

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:
Y

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:
114215
UFC:
63220
LTL:
RATING VARIABLE
LCL:
50.0
WCC:
671
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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