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2840-01-413-0684

Aircraft Gas Turbine Engine Turbine Nozzle Assembly

2840014130684 014130684 4064943CLL 4064943

A stationary item designed for the purpose of directing air at the proper angle and velocity to a ROTOR, TURBINE, AIRCRAFT GAS TURBINE ENGINE. It has provisions for attaching to a CASE (3), TURBINE, AIRCRAFT GAS TURBINE ENGINE. It may have an inner support shroud. The assembled item forms a complete circle. View more Aircraft Gas Turbine Engine Turbine Nozzle Assembly

2840-01-413-0684 NOZZLE ASSEMBLY,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840014130684 014130684

Managed by United States
NSN Created on 4 May 1995
Data Last Changed
January 2023
NATO Update Count
10
NATO Data Quality
2840-01-413-0684 NOZZLE ASSEMBLY,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840014130684 014130684 1/1
NSN 2840-01-413-0684 (Generic Image) 1/1

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2840-01-413-0684 Related Documents Related Documents 2840-01-413-0684 5+ Documents (More...)

4064943CLL 4064943 A stationary item designed for the purpose of directing air at the proper angle and
2840014130684 014130684,4064943CLL,4064943 -01-413-0684Aircraft Gas Turbine Engine Turbine Nozzle https
2840014130684 014130684,4064943CLL,4064943 -01-413-0684Aircraft Gas Turbine Engine Turbine Nozzle Assembly2840014130684
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2840014130684 014130684,4064943CLL,4064943 -01-413-0684Aircraft Gas Turbine Engine Turbine Nozzle
Assembly2840014130684 014130684 4064943CLL 4064943 https//www.nsnlookup.com /fsg-28/fsc-2840/us 2840

2840-01-413-0684 Demil Restrictions 2840-01-413-0684

DEMIL: D | DEMILI: 7 | CRITICALITY: Y | HMIC: N | PMIC: A | EDC: A | ADPEC: 0

2840-01-413-0684 is a Aircraft Gas Turbine Engine Turbine Nozzle Assembly that does not have a nuclear hardened feature, but does have another critical feature or features such as tolerance, fit restriction or application. The DCMO has forced the Demilization requirements for this item as the ICP has not collaborated. 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.

2840-01-413-0684 HTS and ScheduleB Import and Export 2840-01-413-0684

2840-01-413-0684 End Users End Users 2840-01-413-0684

Republic of Korea (ZH01)
Effective Date:
1 Aug 1998
Norway (ZT01)
Effective Date:
1 May 1995

2840-01-413-0684 Manufacturers Approved Sources 2840-01-413-0684

2840-01-413-0684 Technical Data Datasheet 2840-01-413-0684

Characteristic
Specifications
FIIG
A10700
End Item Identification [AGAV]
F100-Pw-220/220E Aircraft Gas Turbine Engine
Criticality Code Justification [CRTL]
Czbj And Czcj And Agav
Engine Section Location [CZBJ]
Turbine
Reference Data And Literature [RDAL]
T.O. 2J-F100-24, Fig 109, Ind 14
Part Name Assigned By Controlling Agency [CXCY]
Original Name Vane,Turbine Engine
Stage Number [CZCJ]
3

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2840-01-413-0684 Freight Data Freight Information 2840-01-413-0684

2840-01-413-0684 has freight characteristics.. 2840-01-413-0684 has a variance between NMFC and UFC when transported by rail and the description should be consulted.

2840-01-413-0684 Packaging Data Packaging Data 2840-01-413-0684

Responsible Activity
Packaging Data Source
Primary Inventory Control Activity (PICA)
--

Item Pack Level (Unpackaged)

Item Size
Item Weight
Characteristics
Weight/Dimensions Category
Fragility
Item Preservation
5.0" H x 4.0" W x 2.0" L
--
--
Over 10lb
Less than 85G
No Requirement

Unit Pack Level (Packaged)

Quantity per Pack
Unit Size
Unit Weight
Unit Cube
Preservation Method
Cleaning/Drying
--
6.3" H x 5.3" W x 4.0" L
--
--
Physical Protection
Any Suitable Process
Preservation Material
Wrapping Material
Cushioning/Dunnage
Cushioning Thickness
Container
Special Marking
No Requirement
--
--
--
PPP-B-1672, Type II, Folding Convoluted Cushioning in Reusable Box
Reusable container

Intermediate Pack Level

Quantity of Unit Packs
Container
ASTM-D5118, Type CF, Class Domestic, Corrugated Fiberboard Box