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2840-01-133-3512

Aircraft Gas Turbine Engine Compressor Rotor

2840011333512 011333512 4044217-711

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

2840-01-133-3512 ROTOR,COMPRESSOR,AIRCRAFT GAS TURBINE ENGINE 2840011333512 011333512

Managed by United States
NSN Created on 12 Jun 1982
Data Last Changed
January 2023
NATO Update Count
11
NATO Data Quality
2840-01-133-3512 ROTOR,COMPRESSOR,AIRCRAFT GAS TURBINE ENGINE 2840011333512 011333512 1/1
NSN 2840-01-133-3512 (Generic Image) 1/1

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2840-01-133-3512 Related Documents Related Documents 2840-01-133-3512 3+ Documents (More...)

RQST NE Updated Every Day 2840-01-133-3512 RQST Updated Every Day 2840-01-133-3512 RQST NE Related Documents
pressure, direction RQST NE Updated Every Day 2840-01-133-3512 RQST Updated Every Day 2840-01-133-3512
2840011333512 011333512,4044217-711 Datasheet 2840-01-133-3512 CharacteristicSpecificationsFIIGA10700End
https//www.nsnlookup.com /fsg-28/fsc-2840/us 2840 https//www.nsnlookup.com /fsg-28/fsc-2840/us 2840-01-133-3512
2840011333512 011333512,4044217-711 Datasheet 2840-01-133-3512 CharacteristicSpecificationsFIIGA10700End
4044217 https//www.nsnlookup.com /fsg-28/fsc-2840/us https//www.nsnlookup.com /fsg-28/fsc-2840/us 2840-01-133-3512
2840011333512 011333512,4044217-711 2840-01-341-6210 Aircraft Gas Turbine Engine Turbine Rotor

2840-01-133-3512 Demil Restrictions 2840-01-133-3512

DEMIL: C | DEMILI: | CRITICALITY: X | HMIC: N | PMIC: U | EDC: | ADPEC: 0

2840-01-133-3512 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. 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. The precious metals content of this item is unknown.

2840-01-133-3512 HTS and ScheduleB Import and Export 2840-01-133-3512

2840-01-133-3512 End Users End Users 2840-01-133-3512

Belgium (ZB01)
Effective Date:
1 Apr 1991
Norway (ZT01)
Effective Date:
1 Apr 1991

2840-01-133-3512 Manufacturers Approved Sources 2840-01-133-3512

2840-01-133-3512 Technical Data Datasheet 2840-01-133-3512

Characteristic
Specifications
FIIG
A10700
End Item Identification [AGAV]
2840-01-117-6058
Fsc Application Data [ZZZV]
Engine,Turbo-Jet
Special Features [FEAT]
Industrial Document,Fscm 77445,Mfr Dwg And Engineering Parts List 4044217-711

2840-01-133-3512 Related Items NATO Stock Numbers Related to 2840-01-133-3512

2840-01-133-3512 Freight Data Freight Information 2840-01-133-3512

2840-01-133-3512 has freight characteristics managed by the Netherlands.It has a National Motor Freight Classification (NMFC) of 123270. A Sub NMFC of Z. It has a NMFC Description of COMPRESSOR REFRIGERATION. 2840-01-133-3512 is rated as a variable freight class when transported by Less-Than Truckload (LTL) freight. 2840-01-133-3512 is rated as class 85 when transported by Less-Than Carload (LCL) rail or ocean freight. It has a Uniform Freight Classification (UFC) number of 62600 which rates the freight between FCL and LCL. 2840-01-133-3512 has a variance between NMFC and UFC when transported by rail and the description should be consulted. It has a Water Commodity Code (WCC) of 593 for ocean manifesting and military sealift. 2840-01-133-3512 is not classified as a special type of cargo when transported by water. 2840-01-133-3512 is not a consolidation and does not exceed 84" in any dimension. It should be compatible with a standard 72" Aircraft Cargo Door when transported by air.