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2840-01-451-9054
Aircraft Gas Turbine Engine Compressor Shroud
2840014519054 014519054 3001462-2
An item within a CASE, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE, designed to surround or partially surround a ROTOR, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE. It's primary purpose is to protect other components of the engine in the event of an impeller or rotor break up. View more Aircraft Gas Turbine Engine Compressor Shroud
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 Restrictions  2840-01-451-9054
2840-01-451-9054 is a Aircraft Gas Turbine Engine Compressor Shroud that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. This item is considered a low risk when released from the control of the Department of Defense. The item may still be subject to the requirements of the Export Administration Regulations (EAR) and the Code of Federal Regulations (CFR). This item is not suspected to be hazardous. This item does not contain a precious metal.
 Import and Export  2840-01-451-9054
- Schedule B
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 - HTS Code
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 End Users  2840-01-451-9054
- US Coast Guard (C057)   
- Effective Date:
  - 1 Jan 1998
 
 Approved Sources  2840-01-451-9054
- Part Number
- Manufacturer
 - Status
 - 3001462-2
  - Manufacturer
 -  99193 - Honeywell International Inc. (Active) 
- Primary Buy
  - Primary Buy
 
 Datasheet  2840-01-451-9054
- Characteristic
- Specifications
 - FIIG
  - Specifications
 - A10700
 - End Item Identification [AGAV]
 - Coast Guard Hu-25A Aircraft
 - Diameter [ABMZ]
 - 14.000 Inches Nominal
 - Engine Section Location [CZBJ]
 - Turbine
 - Material [MATT]
 - Steel Overall
 - Overall Length [ABHP]
 - 14.000 Inches Nominal
 - Overall Width [ABMK]
 - 1.500 Inches Nominal
 - Special Features [FEAT]
 - This Item Is The Exhaust Crossover Duct Shroud Located In The Turbine Section Of The Atf3-6 Turbofan Engine
 
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 Freight Information  2840-01-451-9054
2840-01-451-9054 has freight characteristics.. 2840-01-451-9054 has a variance between NMFC and UFC when transported by rail and the description should be consulted.