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2840-01-027-2425

Aircraft Gas Turbine Engine Compressor Rotor

2840010272425 010272425 108R857G51A

A single or multistage assembly designed to deliver air at the proper pressure, direction and velocity. It consists of disks, blades, hubs, and the like. It is the moving part of COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE. It has facilities for attaching to a SHAFT, TURBINE, AIRCRAFT GAS TURBINE ENGINE. View more Aircraft Gas Turbine Engine Compressor Rotor

2840-01-027-2425 ROTOR,COMPRESSOR,AIRCRAFT GAS TURBINE ENGINE 2840010272425 010272425

Managed by United States
NSN Created on 12 Sep 1976
Data Last Changed
January 2023
NATO Update Count
14
NATO Data Quality
2840-01-027-2425 ROTOR,COMPRESSOR,AIRCRAFT GAS TURBINE ENGINE 2840010272425 010272425 1/1
NSN 2840-01-027-2425 (Generic Image) 1/1

2840-01-027-2425 Stock and Availability Marketplace 2840-01-027-2425

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2840-01-027-2425 Related Documents Related Documents 2840-01-027-2425 1+ Documents (More...)

108R857G51A A single or multistage assembly designed to deliver air at the proper pressure, direction
United States (US) 4. 2840-01-027-2425 Marketplace Restrictions Approved Sources Datasheet Management
RQST NE Updated Every Day 2840-01-027-2425 RQST Updated Every Day 2840-01-027-2425 RQST NE Related Documents

2840-01-027-2425 Demil Restrictions 2840-01-027-2425

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

2840-01-027-2425 is a Aircraft Gas Turbine Engine Compressor Rotor that does not have a nuclear hardened feature, but does have another critical feature or features such as tolerance, fit restriction or application. This item is a US Munitions List or Commerce Control List Item where key elements must be removed and destroyed to prevent this item being restored or repaired. Only authorized parties may possess this item. This item is not suspected to be hazardous. This item does not contain a precious metal.

2840-01-027-2425 HTS and ScheduleB Import and Export 2840-01-027-2425

2840-01-027-2425 End Users End Users 2840-01-027-2425

Spain (YB01)
Effective Date:
1 Apr 1991
Greece (ZU01)
Effective Date:
1 Apr 2008
Turkey (ZW01)
Effective Date:
1 Dec 1995

2840-01-027-2425 Manufacturers Approved Sources 2840-01-027-2425

2840-01-027-2425 Technical Data Datasheet 2840-01-027-2425

Characteristic
Specifications
FIIG
A10700
End Item Identification [AGAV]
Acft Engine J79-15/17
Criticality Code Justification [CRTL]
Agav
Design Type [APGF]
Axial Compressor
Engine Section Location [CZBJ]
Compressor
Special Features [FEAT]
Original Name Compressor Rotor,Axial,Turbine Engine

2840-01-027-2425 Related Items NATO Stock Numbers Related to 2840-01-027-2425

2840-01-027-2425 Freight Data Freight Information 2840-01-027-2425

2840-01-027-2425 has freight characteristics.. 2840-01-027-2425 has a variance between NMFC and UFC when transported by rail and the description should be consulted.