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2840-01-125-3847

Aircraft Gas Turbine Engine Turbine Nozzle Segment

2840011253847 011253847 4059181CLL 4059181

A portion of a NOZZLE ASSEMBLY, TURBINE, AIRCRAFT GAS TURBINE ENGINE. It consists of two or more NOZZLE, TURBINE, AIRCRAFT GAS TURBINE ENGINE cast as one piece. View more Aircraft Gas Turbine Engine Turbine Nozzle Segment

2840-01-125-3847 NOZZLE SEGMENT,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840011253847 011253847

Managed by United States
NSN Created on 26 Jan 1982
Data Last Changed
January 2023
NATO Update Count
23
NATO Data Quality
2840-01-125-3847 NOZZLE SEGMENT,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840011253847 011253847 1/1
NSN 2840-01-125-3847 (Generic Image) 1/1

2840-01-125-3847 Stock and Availability Marketplace 2840-01-125-3847

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2840-01-125-3847 Related Documents Related Documents 2840-01-125-3847 1+ Documents (More...)

4059181CLL 4059181 A portion of a NOZZLE ASSEMBLY, TURBINE, AIRCRAFT GAS TURBINE ENGINE.
United States (US) 4. 2840-01-125-3847 Marketplace Restrictions Approved Sources Datasheet Management
RQST NE Updated Every Day 2840-01-125-3847 RQST Updated Every Day 2840-01-125-3847 RQST NE Related

2840-01-125-3847 Demil Restrictions 2840-01-125-3847

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

2840-01-125-3847 is a Aircraft Gas Turbine Engine Turbine Nozzle Segment 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 Item and must be mutilated to scrap. This item is not suspected to be hazardous. This item does not contain a precious metal.

2840-01-125-3847 HTS and ScheduleB Import and Export 2840-01-125-3847

2840-01-125-3847 End Users End Users 2840-01-125-3847

Belgium (ZB01)
Effective Date:
1 Apr 2003
Norway (ZT01)
Effective Date:
1 Apr 1991
Turkey (ZW01)
Effective Date:
1 Dec 2005

2840-01-125-3847 Manufacturers Approved Sources 2840-01-125-3847

2840-01-125-3847 Technical Data Datasheet 2840-01-125-3847

Characteristic
Specifications
FIIG
A10700
End Item Identification [AGAV]
Acft Eng F100
Criticality Code Justification [CRTL]
Feat
Design Type [APGF]
Axial Compressor
Engine Section Location [CZBJ]
Turbine
Part Name Assigned By Controlling Agency [CXCY]
Original Name Vane,Compressor,Aircraft Gas Turbine Engine
Special Features [FEAT]
T.O. 2J-F100-14, Fig 155, Ind 32; 1.730-1.749 Sq. In. Area; 1800 Cycle; Turbine Stator Support; Replaced By P/Ns 4056781Cll And 4070251Cll
Stage Number [CZCJ]
1

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2840-01-125-3847 Freight Data Freight Information 2840-01-125-3847

2840-01-125-3847 has freight characteristics.. 2840-01-125-3847 has a variance between NMFC and UFC when transported by rail and the description should be consulted.

2840-01-125-3847 Packaging Data Packaging Data 2840-01-125-3847

Responsible Activity
Packaging Data Source
Primary Inventory Control Activity (PICA)
Packaging Data does not meet current MIL-STD-2073-1E

Item Pack Level (Unpackaged)

Item Size
Item Weight
Characteristics
Weight/Dimensions Category
Fragility
Item Preservation
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Unit Pack Level (Packaged)

Quantity per Pack
Unit Size
Unit Weight
Unit Cube
Preservation Method
Cleaning/Drying
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Physical Protection
Any Suitable Process
Preservation Material
Wrapping Material
Cushioning/Dunnage
Cushioning Thickness
Container
Special Marking
No Requirement
No Requirement
No Requirement
Not Applicable
PPP-B-1672, Type II, Folding Convoluted Cushioning in Reusable Box
No special marking

Intermediate Pack Level

Quantity of Unit Packs
Container
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