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2840-01-461-8290

Aircraft Gas Turbine Engine Compressor Rotor

2840014618290 014618290 3070440-11

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

2840-01-461-8290 ROTOR,COMPRESSOR,AIRCRAFT GAS TURBINE ENGINE 2840014618290 014618290

Managed by United States
NSN Created on 6 Jan 1999
Data Last Changed
January 2023
NATO Update Count
3
NATO Data Quality
2840-01-461-8290 ROTOR,COMPRESSOR,AIRCRAFT GAS TURBINE ENGINE 2840014618290 014618290 1/1
NSN 2840-01-461-8290 (Generic Image) 1/1

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2840-01-461-8290 Related Documents Related Documents 2840-01-461-8290 1+ Documents (More...)

3070440-11 A single or multistage assembly designed to deliver air at the proper pressure, direction
United States (US) 4. 2840-01-461-8290 Marketplace Restrictions Approved Sources Datasheet Management
RQST NE Updated Every Day 2840-01-461-8290 RQST Updated Every Day 2840-01-461-8290 RQST NE Related

2840-01-461-8290 Demil Restrictions 2840-01-461-8290

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

2840-01-461-8290 is a Aircraft Gas Turbine Engine Compressor Rotor 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.

2840-01-461-8290 HTS and ScheduleB Import and Export 2840-01-461-8290

2840-01-461-8290 End Users End Users 2840-01-461-8290

Brazil (YA01)
Effective Date:
1 May 2012
Spain (YB01)
Effective Date:
1 Sep 2010
Norway (ZT01)
Effective Date:
1 Jan 1999

2840-01-461-8290 Manufacturers Approved Sources 2840-01-461-8290

2840-01-461-8290 Technical Data Datasheet 2840-01-461-8290

Characteristic
Specifications
FIIG
A10700
Material [MATT]
Steel Overall
Engine Section Location [CZBJ]
Turbine
Reference Data And Literature [RDAL]
72-3560 Service Bulletin
End Item Identification [AGAV]
Next Higher Assembly Tfe 731 Engine
Part Name Assigned By Controlling Agency [CXCY]
Rotor

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2840-01-461-8290 Freight Data Freight Information 2840-01-461-8290

2840-01-461-8290 has freight characteristics.. 2840-01-461-8290 has a variance between NMFC and UFC when transported by rail and the description should be consulted.