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2840-01-088-0923

Aircraft Gas Turbine Engine Turbine Rotor

2840010880923 010880923 7000M19G34 7000M19G23 7000M19G25 7000M19G21 7000M19G27

A single or multistage assembly designed to receive thermal energy from the combustion section and convert it to mechanical energy to drive the ROTOR, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE and/or the ROTOR, FAN, AIRCRAFT GAS TURBINE ENGINE through a SHAFT, TURBINE, AIRCRAFT GAS TURBINE ENGINE. It consists of disks, blades, hubs, and the like. It is the moving part of a TURBINE ASSEMBLY, AIRCRAFT GAS TURBINE ENGINE. It has facilities for attaching to a SHAFT, TURBINE, AIRCRAFT GAS TURBINE ENGINE. View more Aircraft Gas Turbine Engine Turbine Rotor

Managed by United States

NSN Created on 5 Jan 1980

Data Last Changed
January 2023

NATO Update Count
16

NATO Data Quality

2840-01-088-0923 ROTOR,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840010880923 010880923 1/1 — NSN 2840-01-088-0923 (Generic Image) 1/1

Marketplace 2840-01-088-0923

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7000M19G34 ROTOR,TURBINE,AIRCRAFT GAS TURBINE ENGINE 1 EA NS

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2840-01-088-0923 ROTOR,TURBINE,AIRCRAFT GAS TURBINE ENGINE RQST NS

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2840-01-088-0923 RQST NE

Restrictions 2840-01-088-0923

IUID Required

2840-01-088-0923 is a Aircraft Gas Turbine Engine Turbine Rotor that is an aviation critical safety item or flight safety critical aircraft part. 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. This item does not contain a precious metal.

Import and Export 2840-01-088-0923

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End Users 2840-01-088-0923

US Air Force (FXX4)
Effective Date:: 1 Apr 1991; AMC 3 AMSC C AMSC F IMC E IMCACTY SX DSOR FT

Germany (ZG01)
Effective Date:: 1 Apr 1991

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

Greece (ZU01)
Effective Date:: 1 Apr 1991

Approved Sources 2840-01-088-0923

Part Number
Manufacturer
Status
7000M19G34: 07482 - General Electric Company (Active); Primary Buy; RNCC 3 RNVC 2 DAC 2
7000M19G23: 07482 - General Electric Company (Active); Canceled/Obsolete; RNCC 5 RNVC 9 DAC 4
7000M19G25: 07482 - General Electric Company (Active); Canceled/Obsolete; RNCC 5 RNVC 9 DAC 4
7000M19G21: 07482 - General Electric Company (Active); Canceled/Obsolete; RNCC 5 RNVC 9 DAC 4
7000M19G27: 07482 - General Electric Company (Active); Canceled/Obsolete; RNCC 5 RNVC 9 DAC 4

Datasheet 2840-01-088-0923

Characteristic
Specifications
FIIG: A10700
End Item Identification [AGAV]: Acft Eng J79
Criticality Code Justification [CRTL]: Agav

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Freight Information 2840-01-088-0923

2840-01-088-0923 has freight characteristics.It has a National Motor Freight Classification (NMFC) of 114215. A Sub NMFC of Z. It has a NMFC Description of ASSEMBLIES JET AIRCRAFT ENGINE. 2840-01-088-0923 is rated as a variable freight class when transported by Less-Than Truckload (LTL) freight. 2840-01-088-0923 is rated as class 85 when transported by Less-Than Carload (LCL) rail or ocean freight. It has a Uniform Freight Classification (UFC) number of 63220 which rates the freight between FCL and LCL. It has a Water Commodity Code (WCC) of 671 for ocean manifesting and military sealift. 2840-01-088-0923 is not classified as a special type of cargo when transported by water. 2840-01-088-0923 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.

Packaging Data 2840-01-088-0923

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: --; --; --; --; --

Unit Pack Level (Packaged)

Quantity per Pack
Unit Size
Unit Weight
Unit Cube
Preservation Method
Cleaning/Drying: --; 76.5" H x 38.5" W x 48.5" L; --; --; Preservative Coating Only; Any Suitable Process

Preservation Material
Wrapping Material
Cushioning/Dunnage
Cushioning Thickness
Container
Special Marking: MIL-PRF-23827, Grease, Aircraft and Instrument, Gear and Actuator Screw; Special Requirements – see Specific Instructions or Drawings provided; Special Requirements. See Specific Instructions or Drawings Provided; Special Requirements. See Specific Instructions or Drawings Provided; Special requirement – See specific instructions or drawings provided; Special requirements

Intermediate Pack Level

Quantity of Unit Packs
Container: --; No Requirement