Model: 9521M23G02

Turbine Engine Afterburner

Properties:

End Application
Aircraft eng f110
Criticality Code Justification
Agav
NSN
2840-01-190-9907
Part Number
9521M23G02
Description
Afterburner,turbine Engine
CAGE
07482

A chamber in which additional fuel is injected into, the exhaust gases, and reheating the gases to develop increased thrust. It consists of combustion area, flame holders, injection nozzles and an exhaust ejector.

Part 9521M23G02 NSN 2840-01-190-9907

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
60031
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:
PR
CRITL:
Y

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
48.0 X 48.0 X 29.5
Paclk Weight:
322.0000lbs
Item Weight:
195.0000lbs
Item Dim:
041004100218
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
A
SPI No.:
F011909907
SPI Rev.:
E
SPC Mkg:
ZZ
LVL_A:
LVL_B:

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
114030
UFC:
64100
LTL:
200.0
LCL:
RATING VARIABLE
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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