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2840-01-448-7512

Aircraft Gas Turbine Engine Compressor Vane Assembly

2840014487512 014487512 4084343CLN 4084343

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

2840-01-448-7512 VANE ASSEMBLY,COMPRESSOR,AIRCRAFT GAS TURBINE ENGINE 2840014487512 014487512

Managed by United States
NSN Created on 9 Sep 1997
Data Last Changed
January 2023
NATO Update Count
5
NATO Data Quality
2840-01-448-7512 VANE ASSEMBLY,COMPRESSOR,AIRCRAFT GAS TURBINE ENGINE 2840014487512 014487512 1/1
NSN 2840-01-448-7512 (Generic Image) 1/1

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2840-01-448-7512 Related Documents Related Documents 2840-01-448-7512 5+ Documents (More...)

4084343CLN 4084343 A stationary item designed for the purpose of directing air at the proper angle and
United States (US) 4. 2840-01-448-7512 Marketplace Restrictions Approved Sources Datasheet Management
RQST NE Updated Every Day 2840-01-448-7512 RQST Updated Every Day 2840-01-448-7512 RQST NE Related Documents
01-448-4904Aircraft Gas Turbine Engine Compressor Vane Assembly2840014484904 014484904 4084343CLL 4084343
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01-448-6993Aircraft Gas Turbine Engine Compressor Vane Assembly2840014486993 014486993 4084343CLR 4084343
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01-448-6995Aircraft Gas Turbine Engine Compressor Vane Assembly2840014486995 014486995 4084343CLS 4084343
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2840-01-448-7512 Demil Restrictions 2840-01-448-7512

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

2840-01-448-7512 is a Aircraft Gas Turbine Engine Compressor Vane Assembly 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.

2840-01-448-7512 HTS and ScheduleB Import and Export 2840-01-448-7512

2840-01-448-7512 End Users End Users 2840-01-448-7512

Belgium (ZB01)
Effective Date:
1 Sep 1998

2840-01-448-7512 Manufacturers Approved Sources 2840-01-448-7512

2840-01-448-7512 Technical Data Datasheet 2840-01-448-7512

Characteristic
Specifications
FIIG
A10700
End Item Identification [AGAV]
F100-Pw-220 Aircraft Gas Turbine Engine
Criticality Code Justification [CRTL]
Czbj And Abhp And Abmz And Abmk And Feat
Design Type [APGF]
Axial Compressor
Diameter [ABMZ]
13.410 Inches Minimum And 13.450 Inches Maximum
Engine Section Location [CZBJ]
Turbine
Overall Length [ABHP]
4.717 Inches Minimum And 4.737 Inches Maximum
Overall Width [ABMK]
2.036 Inches Minimum And 2.084 Inches Maximum
Part Name Assigned By Controlling Agency [CXCY]
Original Name Vane,Turbine Statorassembly
Special Features [FEAT]
4.639-4.664 Square Inch Flow Area
Stage Number [CZCJ]
3

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2840-01-448-7512 Freight Data Freight Information 2840-01-448-7512

2840-01-448-7512 has freight characteristics.It has a National Motor Freight Classification (NMFC) of 133300. A Sub NMFC of Z. It has a NMFC Description of MACHINERY/MACHINES NOI. 2840-01-448-7512 is rated as a variable freight class when transported by Less-Than Truckload (LTL) freight. It has a Uniform Freight Classification (UFC) number of 63220 which rates the freight between FCL and LCL. 2840-01-448-7512 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. 2840-01-448-7512 is not classified as a special type of cargo when transported by water. 2840-01-448-7512 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.