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2840-01-047-3442

Aircraft Gas Turbine Engine Turbine Rotor Blade

2840010473442 010473442 6890506

An item mounted on a DISK, TURBINE, AIRCRAFT GAS TURBINE ENGINE. It is designed to create the flow of air in the turbine section of an ENGINE, GAS TURBINE, AIRCRAFT. View more Aircraft Gas Turbine Engine Turbine Rotor Blade

Managed by United States

NSN Created on 5 Sep 1977

Data Last Changed
January 2023

NATO Update Count
30

NATO Data Quality

2840-01-047-3442 BLADE,TURBINE ROTOR,AIRCRAFT GAS TURBINE ENGINE 2840010473442 010473442 1/1 — NSN 2840-01-047-3442 (Generic Image) 1/1

Marketplace 2840-01-047-3442

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6890506 BLADE,TURBINE ROTOR,AIRCRAFT GAS TURBINE ENGINE 100 EA NS

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6890506 BLADE,TURBINE ROTOR,AIRCRAFT GAS TURBINE ENGINE 26 EA NS

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2840-01-047-3442 RQST NE

Restrictions 2840-01-047-3442

2840-01-047-3442 is a Aircraft Gas Turbine Engine Turbine Rotor Blade 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 2840-01-047-3442

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End Users 2840-01-047-3442

Brazil (YA01)
Effective Date:: 1 Jan 2011

Spain (YB01)
Effective Date:: 1 Apr 1991

Singapore (YJ01)
Effective Date:: 1 Apr 1991

Canada (ZC01)
Effective Date:: 1 May 2013

New Zealand (ZE01)
Effective Date:: 1 Apr 1991

Germany (ZG01)
Effective Date:: 1 Mar 2013

Republic of Korea (ZH01)
Effective Date:: 1 Jun 1996

United Kingdom (ZK01)
Effective Date:: 1 Apr 1991

Portugal (ZP01)
Effective Date:: 1 Jun 2014

Italy (ZR01)
Effective Date:: 1 Dec 2007

Norway (ZT01)
Effective Date:: 1 Apr 1991

Greece (ZU01)
Effective Date:: 1 Apr 2008

Approved Sources 2840-01-047-3442

Part Number
Manufacturer
Status
6890506: 63005 - Rolls-Royce Corporation (Active); Primary Buy; RNCC 3 RNVC 2 DAC 2
6890506: 73342 - Allison Transmission Inc (Active); Canceled/Obsolete; RNCC 5 RNVC 9 DAC 2

Datasheet 2840-01-047-3442

Characteristic
Specifications
FIIG: A10700
End Item Identification [AGAV]: Aircraft Engine,T-56
Criticality Code Justification [CRTL]: Agav
Engine Section Location [CZBJ]: Turbine
Material [MATT]: Steel Corrosion Resisting Blade
Material Document And Classification [MDCL]: Ems73657 Assn Std Single Material Response Blade

NATO Stock Numbers Related to 2840-01-047-3442

2840-14-552-0446 2840-66-092-4372 2840-14-320-7921 2840-14-428-6754 2840-14-031-3722 2840-14-428-6747 2840-14-404-0950 2840-14-330-4426 2840-14-322-2335 2840-01-518-6724 2840-99-710-4922 2840-14-339-6172 2840-14-339-6171 2840-14-471-0373 2840-99-192-5084 2840-12-375-2627 2840-01-038-9083 2840-14-416-9304

Freight Information 2840-01-047-3442

2840-01-047-3442 has freight characteristics.. 2840-01-047-3442 has a variance between NMFC and UFC when transported by rail and the description should be consulted.

Packaging Data 2840-01-047-3442

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: --; --; Bare Metal Item; Over 10lb; Less than 85G; No Requirement

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; --; --; --; Any Suitable Container; --

Intermediate Pack Level

Quantity of Unit Packs
Container: PPP-B-566, PPP-B-676, or ASTM-D5118, Folding, Setup or Fiberboard Box