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2840-01-125-3853

Aircraft Gas Turbine Engine Turbine Nozzle Segment

2840011253853 011253853 4056781CLL 4056781

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

2840-01-125-3853 NOZZLE SEGMENT,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840011253853 011253853

Managed by United States
NSN Created on 26 Jan 1982
Data Last Changed
January 2023
NATO Update Count
26
NATO Data Quality
2840-01-125-3853 NOZZLE SEGMENT,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840011253853 011253853 1/1
NSN 2840-01-125-3853 (Generic Image) 1/1

2840-01-125-3853 Stock and Availability Marketplace 2840-01-125-3853

2840-01-125-3853 Related Documents Related Documents 2840-01-125-3853 1+ Documents (More...)

4056781CLL 4056781 A portion of a NOZZLE ASSEMBLY, TURBINE, AIRCRAFT GAS TURBINE ENGINE.
United States (US) 4. 2840-01-125-3853 Marketplace Restrictions Approved Sources Datasheet Management
RQST NE Related Documents 2840-01-125-3853 1+ Documents ( More... ) https//www.nsnlookup.com /fsg

2840-01-125-3853 Demil Restrictions 2840-01-125-3853

DEMIL: D | DEMILI: | CRITICALITY: F | HMIC: N | PMIC: A | EDC: | ADPEC:

2840-01-125-3853 is a Aircraft Gas Turbine Engine Turbine Nozzle Segment that is an aviation critical safety item or flight safety critical aircraft part. 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.

2840-01-125-3853 HTS and ScheduleB Import and Export 2840-01-125-3853

2840-01-125-3853 End Users End Users 2840-01-125-3853

Belgium (ZB01)
Effective Date:
1 Apr 2003
Republic of Korea (ZH01)
Effective Date:
1 Apr 1991
Norway (ZT01)
Effective Date:
1 Apr 1991

2840-01-125-3853 Manufacturers Approved Sources 2840-01-125-3853

2840-01-125-3853 Technical Data Datasheet 2840-01-125-3853

Characteristic
Specifications
FIIG
A10700
End Item Identification [AGAV]
Acft Eng F100
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 Inch Area; Turbine Stator Support; 1800 Cycle; Replaces P/N 4056781Cll; Replaced By 4070251Cll
Stage Number [CZCJ]
1

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2840-01-125-3853 Freight Data Freight Information 2840-01-125-3853

2840-01-125-3853 has freight characteristics.. 2840-01-125-3853 has a variance between NMFC and UFC when transported by rail and the description should be consulted.

2840-01-125-3853 Packaging Data Packaging Data 2840-01-125-3853

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
--
--
--
--
--

Unit Pack Level (Packaged)

Quantity per Pack
Unit Size
Unit Weight
Unit Cube
Preservation Method
Cleaning/Drying
--
--
--
--
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
ASTM-D5118, Type CF, Class Domestic, Corrugated Fiberboard Box