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2840-01-612-0143
Turbine Engine Cooling Plate
2840016120143 016120143 6068T36P04
An item of various cross sections used to exhaust heat from the gas generator turbine rotor of a turbine engine. View more Turbine Engine Cooling Plate
January 2023
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Related Documents 2840-01-612-0143 1+ Documents (More...)
/fsc-2840/us 2840-01-612-0143 Turbine Engine Cooling Plate 2840016120143 6068T36P04 An item of various
Restrictions 2840-01-612-0143 DEMIL: D | DEMILI : 1 | CRITICALITY : X | HMIC : N | PMIC : A | EDC
Restrictions 2840-01-612-0143
2840-01-612-0143 is a Turbine Engine Cooling Plate that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. Demilitarization of this item has been confirmed and is not currently subject to changes. This item is a US Munitions List or Commerce Control List Item which must be destroyed to prevent restoration or repair. Only authorized parties may possess this item. This item is not suspected to be hazardous. This item does not contain a precious metal.
Import and Export 2840-01-612-0143
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 2840-01-612-0143
- Spain (YB01)
- Effective Date:
- 1 Oct 2012
Approved Sources 2840-01-612-0143
- Part Number
- Manufacturer
- Status
- 6068T36P04
- Manufacturer
- 99204 - De Coursey Engineering Laboratory (Active)
- Primary Buy
- Primary Buy
Datasheet 2840-01-612-0143
- Characteristic
- Specifications
- FIIG
- Specifications
- A23900
- Special Features [FEAT]
- 72-41-00 Rotor Assembly-Stages 1 And 2 Low Stress Gas Generator Turbine,Plate Stage 2 Turbine Aft Cooling, This Item Has Replaced 6068T36p01.
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Freight Information 2840-01-612-0143
2840-01-612-0143 has freight characteristics.. 2840-01-612-0143 has a variance between NMFC and UFC when transported by rail and the description should be consulted.