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2840-01-508-4623

Aircraft Gas Turbine Engine Fan Shroud

2840015084623 015084623 212-070-137-18

An item within a CASE, FAN, AIRCRAFT GAS TURBINE ENGINE, designed to surround or partially surround a ROTOR, FAN, 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 Fan Shroud

2840-01-508-4623 SHROUD,FAN,AIRCRAFT GAS TURBINE ENGINE 2840015084623 015084623

Managed by United States
NSN Created on 21 May 2003
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
2840-01-508-4623 SHROUD,FAN,AIRCRAFT GAS TURBINE ENGINE 2840015084623 015084623 1/1
NSN 2840-01-508-4623 (Generic Image) 1/1

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2840-01-508-4623 Demil Restrictions 2840-01-508-4623

DEMIL: A | DEMILI: 1 | CRITICALITY: X | HMIC: N | PMIC: A | EDC: A | ADPEC: 0

2840-01-508-4623 is a Aircraft Gas Turbine Engine Fan Shroud 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 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.

2840-01-508-4623 HTS and ScheduleB Import and Export 2840-01-508-4623

2840-01-508-4623 End Users End Users 2840-01-508-4623

Italy (ZR)
Italy (ZR01)
Effective Date:
1 May 2003

2840-01-508-4623 Manufacturers Approved Sources 2840-01-508-4623

2840-01-508-4623 Technical Data Datasheet 2840-01-508-4623

Characteristic
Specifications
FIIG
A10700
End Item Identification [AGAV]
Helicopter

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2840-01-508-4623 Freight Data Freight Information 2840-01-508-4623

2840-01-508-4623 has freight characteristics.. 2840-01-508-4623 has a variance between NMFC and UFC when transported by rail and the description should be consulted.