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2840-01-375-1408

Aircraft Gas Turbine Engine Compressor Blade

2840013751408 013751408 4080621 4080531 4080541 4080601 4080701

An item mounted on a DISK, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE. It is designed to create the flow of air in the compressor section of an ENGINE, GAS TURBINE, AIRCRAFT. View more Aircraft Gas Turbine Engine Compressor Blade

2840-01-375-1408 BLADE,COMPRESSOR,AIRCRAFT GAS TURBINE ENGINE 2840013751408 013751408

Managed by United States
NSN Created on 6 May 1993
Data Last Changed
January 2023
NATO Update Count
11
NATO Data Quality
2840-01-375-1408 BLADE,COMPRESSOR,AIRCRAFT GAS TURBINE ENGINE 2840013751408 013751408 1/1
NSN 2840-01-375-1408 (Generic Image) 1/1

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2840-01-375-1408 Related Documents Related Documents 2840-01-375-1408 5+ Documents (More...)

instructions how to enable JavaScript in your web browser . 6115-15-131-4932Tasselli6115151314932 151314932 4080701
994080701 2540-99-408-0701 2540994080701 994080701 https//www.nsnlookup.com /fsg-28/fsc-2840/us 2840-01-375-1408
2840013751408 013751408,4080621,4080531 1408Aircraft Gas Turbine Engine Compressor Blade2840013751408
5998-00-408-0701 5998004080701 004080701 is a grouping of two or more different types of electrical/electronic components mounted on a common mounting. it may include an assembly of electrical/electronic components mounted on multiple printed wiring board(s) mounted back to back, stacked, and the like. the item is generally a component of a subassembly and cannot be assigned a more definite item name. excludes items which may be identified as a subassembly. for an assembly of electrical/electronic components mounted on a single printed wiring board, see circuit card asseembly. do not use if a more specific name applies.
6030-01-408-0701 6030014080701 014080701 is a device which accepts optic signals and converts them to electrical or radio frequency. it accommodates voltage and optics and is immune to electromagnetic interference (emi) and radio frequency interference (rfi) that is generated. it connects data terminal equipment to a fiber optic transmission line or network.

2840-01-375-1408 Demil Restrictions 2840-01-375-1408

DEMIL: Q | DEMILI: 3 | CRITICALITY: Y | HMIC: N | PMIC: A | EDC: | ADPEC: 0

2840-01-375-1408 is a Aircraft Gas Turbine Engine Compressor Blade 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 has been confirmed as a Critical Munitions List Item or a Sensitive Commerce Control List Item and cannot be in the possession of any party anywhere in the World who is not an authorized NATO Government. Any other possessor of this item should mutilate it now as possession violates international and local laws. This item is a confirmed Commerce Control List Item (CCLI). This item is not suspected to be hazardous. This item does not contain a precious metal.

2840-01-375-1408 HTS and ScheduleB Import and Export 2840-01-375-1408

2840-01-375-1408 End Users End Users 2840-01-375-1408

Belgium (ZB01)
Effective Date:
1 May 1996

2840-01-375-1408 Manufacturers Approved Sources 2840-01-375-1408

2840-01-375-1408 Technical Data Datasheet 2840-01-375-1408

Characteristic
Specifications
FIIG
A10700
Engine Section Location [CZBJ]
Compressor
Stage Number [CZCJ]
1
Blade Attachment Method [BGLW]
Lock
Special Features [FEAT]
T.O. 2J-F100-14
Criticality Code Justification [CRTL]
Agav
End Item Identification [AGAV]
F100pw100/200/220 Acft Engines

2840-01-375-1408 Related Items NATO Stock Numbers Related to 2840-01-375-1408

2840-01-375-1408 Freight Data Freight Information 2840-01-375-1408

2840-01-375-1408 has freight characteristics.. 2840-01-375-1408 has a variance between NMFC and UFC when transported by rail and the description should be consulted.