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2840-00-723-2337

Aircraft Gas Turbine Engine Antifriction Bearing Housing

2840007232337 007232337 646C687P1

A housing designed to surround, retain, support, and protect an antifriction bearing mounted on a SHAFT, TURBINE, AIRCRAFT GAS TURBINE ENGINE. It may also act as a sump to collect the lubricant to be pumped back to the tank. View more Aircraft Gas Turbine Engine Antifriction Bearing Housing

Managed by United States

NSN Created on 1 Jan 1963

Data Last Changed
January 2023

NATO Update Count
28

NATO Data Quality

2840-00-723-2337 HOUSING,ANTIFRICTION BEARING,AIRCRAFT GAS TURBINE ENGINE 2840007232337 007232337 1/1 — NSN 2840-00-723-2337 (Generic Image) 1/1

Marketplace 2840-00-723-2337

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2840-00-723-2337 RQST NE

Restrictions 2840-00-723-2337

2840-00-723-2337 is a Aircraft Gas Turbine Engine Antifriction Bearing Housing that does not have a nuclear hardened feature, but does have another critical feature or features such as tolerance, fit restriction or application. Demilitarization of this item has been confirmed and is not currently subject to changes. 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. The precious metals content of this item is unknown.

Import and Export 2840-00-723-2337

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HTS Code: Subscribe to View HTS Code

End Users 2840-00-723-2337

Brazil (YA01)
Effective Date:: 1 Sep 2007

Spain (YB01)
Effective Date:: 1 Apr 1991

Malaysia (YW01)
Effective Date:: 1 Mar 1995

Republic of Korea (ZH01)
Effective Date:: 1 Apr 1991

Italy (ZR01)
Effective Date:: 1 Dec 2007

Greece (ZU01)
Effective Date:: 1 Apr 1991

Turkey (ZW01)
Effective Date:: 1 Nov 2005

Approved Sources 2840-00-723-2337

Part Number
Manufacturer
Status
646C687P1: 99207 - General Electric Company (Active); Primary Buy; RNCC 3 RNVC 2 DAC 5
646C687P1: 24446 - General Electric Company (Active); Canceled/Obsolete; RNCC 5 RNVC 9 DAC 5

Datasheet 2840-00-723-2337

Characteristic
Specifications
FIIG: A530F0
End Item Identification [AGAV]: J-85 Aircraft Engine
Criticality Code Justification [CRTL]: Agav
Diameter [ABMZ]: 2.240 Inches Minimum And 2.250 Inches Maximum
Engine Section Location [CZBJ]: Turbine
Material [MATT]: Steel Overall
Overall Length [ABHP]: 1.686 Inches Nominal

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Freight Information 2840-00-723-2337

2840-00-723-2337 has freight characteristics.. 2840-00-723-2337 has a variance between NMFC and UFC when transported by rail and the description should be consulted.

Packaging Data 2840-00-723-2337

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: --; --; --; --; Preservative Coating Only; Any Suitable Process

Preservation Material
Wrapping Material
Cushioning/Dunnage
Cushioning Thickness
Container
Special Marking: MIL-PRF-16173, Grade 2, Corrosion Preventive, Solvent Cutback, Cold Application, Soft Film; MIL-PRF-121, Greaseproof, Waterproof Barrier; PPP-C-795, Cellular Plastic Film Cushioning; or A-A-3129, Open Cell Plastic Cushioning; or PPP-C-1797, Polypropylene Foam Cushioning; or A-A-59136, Polyethylene Foam Cushioning; --; PPP-B-566, Folding Paperboard Box; --

Intermediate Pack Level

Quantity of Unit Packs
Container: No Requirement