2840-21-911-0228

Aircraft Gas Turbine Engine Turbine Rotor

2840219110228 219110228 5003T33G08 5003T33G17 5003T33G14 5003T33G12

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

2840-21-911-0228 ROTOR,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840219110228 219110228

Managed by Canada
NSN Created on 20 Aug 1993
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
2840-21-911-0228 ROTOR,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840219110228 219110228 1/1
NSN 2840-21-911-0228 (Generic Image) 1/1

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Account Upgrade 2840-00-411-7780Aircraft Gas Turbine Engine Turbine Rotor2840004117780 004117780 5003T33G17
5003T33G12 A single or multistage assembly designed to receive thermal energy from the combustion section
a Quotation from participating marketplace vendors Request Subscribe to View Vendor Details... 5003T33G12
Upgrade your Account Upgrade 2840-00-088-6796Turbine Engine Turbine Rotor2840000886796 000886796 5003T33G08
Upgrade your Account Upgrade 2840-00-258-2910Turbine Engine Turbine Rotor2840002582910 002582910 5003T33G14
1966 5315-21-845-9066 Headless Straight Pin 6003T13P36RNCC: 3 | RNVC: 2 | DAC: 6 14 Feb 1967 2840-21-911-0228

2840-21-911-0228 Demil Restrictions 2840-21-911-0228

DEMIL: | DEMILI: | CRITICALITY: | HMIC: | PMIC: | EDC: | ADPEC:

2840-21-911-0228 is a Aircraft Gas Turbine Engine Turbine Rotor

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