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2840-01-447-4918

Aircraft Gas Turbine Engine Turbine Nozzle Assembly

2840014474918 014474918 4084243CLR 4084243

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

Managed by United States

NSN Created on 7 Aug 1997

Data Last Changed
January 2023

NATO Update Count
11

NATO Data Quality

2840-01-447-4918 NOZZLE ASSEMBLY,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840014474918 014474918 1/1 — NSN 2840-01-447-4918 (Generic Image) 1/1

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2840-01-447-4918 2840014474918 014474918,4084243CLR,4084243

4084243CLR 4084243 A stationary item designed for the purpose of directing air at the proper angle and
United States (US) 4. 2840-01-447-4918 Marketplace Restrictions Approved Sources Datasheet Management
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2840-01-447-4915 2840014474915 014474915,4084243CLP,4084243

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Restrictions 2840-01-447-4918

2840-01-447-4918 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. 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.

Import and Export 2840-01-447-4918

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End Users 2840-01-447-4918

Singapore (YJ01)
Effective Date:: 1 Sep 1998

Republic of Korea (ZH01)
Effective Date:: 1 Aug 1998

Denmark (ZS01)
Effective Date:: 1 Mar 2013

Norway (ZT01)
Effective Date:: 1 Jun 1998

Approved Sources 2840-01-447-4918

Part Number
Manufacturer
Status
4084243CLR: 77445 - Rtx Corporation (Active); Primary Buy; RNCC 3 RNVC 2 DAC 2
4084243: 77445 - Rtx Corporation (Active); Informational Drawing; RNCC D RNVC 9 DAC 2

Datasheet 2840-01-447-4918

Characteristic
Specifications
FIIG: A10700
End Item Identification [AGAV]: F100-Pw-100/200 Aircraft Gas Turbine Engine
Blade Attachment Method [BGLW]: Slot
Criticality Code Justification [CRTL]: Matt And Abkw And Abmk And Abhp And Feat
Design Type [APGF]: Axial Compressor
Diameter [ABMZ]: 13.410 Inches Minimum And 13.450 Inches Maximum
Engine Section Location [CZBJ]: Low Pressure Turbine
Material [MATT]: Nickel Alloy Overall
Overall Height [ABKW]: 4.717 Inches Minimum And 4.737 Inches Maximum
Overall Length [ABHP]: 2.820 Inches Nominal
Overall Width [ABMK]: 2.036 Inches Minimum And 2.084 Inches Maximum
Part Name Assigned By Controlling Agency [CXCY]: Original Name Vane, Turbine Stator
Special Features [FEAT]: T.O. 2J-F100-24, Fig 109; Flow Area 4.689-4.714 Square Inch Area
Stage Number [CZCJ]: 3

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Freight Information 2840-01-447-4918

2840-01-447-4918 has freight characteristics.. 2840-01-447-4918 has a variance between NMFC and UFC when transported by rail and the description should be consulted.

Packaging Data 2840-01-447-4918

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: 4.8" H x 3.6" 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