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2840-01-484-2339

Aircraft Gas Turbine Engine Compressor Shroud

2840014842339 014842339 4319854-02

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

2840-01-484-2339 SHROUD,COMPRESSOR,AIRCRAFT GAS TURBINE ENGINE 2840014842339 014842339

Managed by United States
NSN Created on 23 Apr 2001
Data Last Changed
January 2023
NATO Update Count
2
NATO Data Quality
2840-01-484-2339 SHROUD,COMPRESSOR,AIRCRAFT GAS TURBINE ENGINE 2840014842339 014842339 1/1
NSN 2840-01-484-2339 (Generic Image) 1/1

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2840-01-484-2339 Related Documents Related Documents 2840-01-484-2339 1+ Documents (More...)

United States (US) 4. 2840-01-484-2339 Marketplace Restrictions Approved Sources Datasheet Management
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2840-01-484-2339 Demil Restrictions 2840-01-484-2339

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

2840-01-484-2339 is a Aircraft Gas Turbine Engine Compressor Shroud that does not have a nuclear hardened feature, but does have another critical feature or features 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.

2840-01-484-2339 HTS and ScheduleB Import and Export 2840-01-484-2339

2840-01-484-2339 End Users End Users 2840-01-484-2339

Federal Bureau of Investigation (FDD4)
Effective Date:
1 May 2013
Former MOE Rule:
FDD5

2840-01-484-2339 Manufacturers Approved Sources 2840-01-484-2339

2840-01-484-2339 Technical Data Datasheet 2840-01-484-2339

Characteristic
Specifications
FIIG
A10700
Criticality Code Justification [CRTL]
Agav
End Item Identification [AGAV]
F119-Pw-100 Engine On F-22 Aircraft
Part Name Assigned By Controlling Agency [CXCY]
Shroud Segment Compressor Stator 4 Stage

2840-01-484-2339 Management Data Management Data 2840-01-484-2339

Effective Date
Organization
Unit of Issue
Unit Price
Qty Unit Pack
May 2013
Department of the Air Force (DF)
EA
Subscribe
1

Air Force Air Force

Budget:
S
57X3010 - Aircraft Replenishment Spares
Aggregation Code:
RF
F-119-PW-100 FOR ATF-ENGINE
Price Validation Code:
E
The current standard price is an estimated price.
Estimated Price challenges are allowed but follow procedures in para 60.b. (3) of section L of this manual.
This code will be changed to a P code upon notification of a contract price or this code will be changed to an updated code upon determination of a valid price.
Expendability
Recoverability
Repairability:
T
Expendable. Reparable. Condemn at Depot. AF Recoverable Assembly Management System (AFRAMS).

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2840-01-484-2339 Freight Data Freight Information 2840-01-484-2339

2840-01-484-2339 has freight characteristics.. 2840-01-484-2339 has a variance between NMFC and UFC when transported by rail and the description should be consulted.