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2840-01-484-5564

Aircraft Gas Turbine Engine Diffuser Case Plug

2840014845564 014845564 4321065

A usually round item of various cross sections designed for temporary installation into a hole in a CASE, DIFFUSER, AIRCRAFT GAS TURBINE ENGINE for the purpose of preventing air from escaping during engine operation. When removed, the hole is for inserting inspection probes, borescopes and the like. It may be grooved or tapered for installation and removal. It may include spacers, springs, rivets and the like. View more Aircraft Gas Turbine Engine Diffuser Case Plug

2840-01-484-5564 PLUG,DIFFUSER CASE,AIRCRAFT GAS TURBINE ENGINE 2840014845564 014845564

Managed by United States
NSN Created on 1 May 2001
Data Last Changed
January 2023
NATO Update Count
3
NATO Data Quality
2840-01-484-5564 PLUG,DIFFUSER CASE,AIRCRAFT GAS TURBINE ENGINE 2840014845564 014845564 1/1
NSN 2840-01-484-5564 (Generic Image) 1/1

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2840-01-484-5564 Related Documents Related Documents 2840-01-484-5564 5+ Documents (More...)

4321065 A usually round item of various cross sections designed for temporary installation into a hole
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2840-01-484-5564 DEMIL: D | DEMILI : 1 | CRITICALITY : Y | HMIC : N | PMIC : A | EDC: | ADPEC : 0 2840
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2840-01-484-5564 Demil Restrictions 2840-01-484-5564

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

2840-01-484-5564 is a Aircraft Gas Turbine Engine Diffuser Case Plug 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 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.

2840-01-484-5564 HTS and ScheduleB Import and Export 2840-01-484-5564

2840-01-484-5564 End Users End Users 2840-01-484-5564

Federal Bureau of Investigation (FDD5)
Effective Date:
1 May 2001

2840-01-484-5564 Manufacturers Approved Sources 2840-01-484-5564

2840-01-484-5564 Technical Data Datasheet 2840-01-484-5564

Characteristic
Specifications
FIIG
A525D0
Special Features [FEAT]
Ap 8 (3 Each) Provides Access Between 9Th-Stage Rotor,Exit Guide Vanes,And Diffuser; To Hpt Vanes,Inside Diameter (Id) And Outside Diamter (Od) Of Combustor;And Gas Generator (Gg) Fuel Nozzles, And Lpt Vanes
Criticality Code Justification [CRTL]
Agav
End Item Identification [AGAV]
F119-Pw-100 Engine On F-22 Aircraft
Part Name Assigned By Controlling Agency [CXCY]
Plug Assy Of--Instrumentation Boss (Ap 8)

2840-01-484-5564 Management Data Management Data 2840-01-484-5564

Effective Date
Organization
Unit of Issue
Unit Price
Qty Unit Pack
Jan 2014
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:
N
Expendable. Condemn at User. Stock Fund (except Munitions).

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2840-01-484-5564 Freight Data Freight Information 2840-01-484-5564

2840-01-484-5564 has freight characteristics.. 2840-01-484-5564 has a variance between NMFC and UFC when transported by rail and the description should be consulted.