2840-01-447-5137

Aircraft Gas Turbine Engine Turbine Rotor

2840014475137 014475137 166119-100A

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

2840-01-447-5137 ROTOR,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840014475137 014475137

Managed by United States
NSN Created on 8 Aug 1997
Data Last Changed
November 2023
NATO Update Count
3
NATO Data Quality
2840-01-447-5137 ROTOR,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840014475137 014475137 1/1
NSN 2840-01-447-5137 (Generic Image) 1/1

2840-01-447-5137 Stock and Availability Marketplace 2840-01-447-5137

Need Help?
Request a Quotation from participating marketplace vendors
eBay Updated Every Day
2840-01-447-5137 RQST NE eBay
eBay Updated Every Day
2840-01-447-5137 RQST eBay
Amazon Updated Every Day
2840-01-447-5137 RQST NE Amazon

2840-01-447-5137 Related Documents Related Documents 2840-01-447-5137 5+ Documents (More...)

2840-01-445-7505 2840014457505 014457505 is 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.
2840-01-551-4792 2840015514792 015514792 is 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.
2840-01-665-0986 2840016650986 016650986 is 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.
DAC: 5 1 Jan 1960 5340-01-447-3115 Access Cover 171104-1RNCC: 3 | RNVC: 2 | DAC: B 1 Aug 1997 2840-01-447-5137

2840-01-447-5137 Demil Restrictions 2840-01-447-5137

DEMIL: Q | DEMILI: 6 | CRITICALITY: X | HMIC: N | PMIC: A | EDC: A | ADPEC: 0

2840-01-447-5137 is a Aircraft Gas Turbine Engine Turbine Rotor that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. This item has been confirmed as a Non-Critical Munitions List Item or a Non-Sensitive Commerce Control List Item and cannnot be in the possession of any party outside of the USA who is a not an authorized NATO Government. Any other possessor of this item should mutilate it now as possession violates international and local laws. This item is a confirmed Commerce Control List Item (CCLI). This item is not suspected to be hazardous. This item does not contain a precious metal.

2840-01-447-5137 Manufacturers Approved Sources 2840-01-447-5137

2840-01-447-5137 Related Items NATO Stock Numbers Related to 2840-01-447-5137