2835-01-413-0217

Nonaircraft Gas Turbine Engine Turbine Rotor

2835014130217 014130217 501E123ED-P-63

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, NONAIRCRAFT GAS TURBINE ENGINE and/or the ROTOR, FAN, NONAIRCRAFT GAS TURBINE ENGINE through a SHAFT, TURBINE, NONAIRCRAFT GAS TURBINE ENGINE. It consists of disks, blades, hubs, and the like. It is the moving part of a TURBINE ASSEMBLY, NONAIRCRAFT GAS TURBINE ENGINE. It has facilities for attaching to a SHAFT, TURBINE, NONAIRCRAFT GAS TURBINE ENGINE. View more Nonaircraft Gas Turbine Engine Turbine Rotor

2835-01-413-0217 ROTOR,TURBINE,NONAIRCRAFT GAS TURBINE ENGINE 2835014130217 014130217

Managed by United States
NSN Created on 4 May 1995
Data Last Changed
November 2023
NATO Update Count
3
NATO Data Quality
2835-01-413-0217 ROTOR,TURBINE,NONAIRCRAFT GAS TURBINE ENGINE 2835014130217 014130217 1/1
NSN 2835-01-413-0217 (Generic Image) 1/1

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501E123ED-P-63 A single or multistage assembly designed to receive thermal energy from the combustion
United States (US) 4. 2835-01-413-0217 Marketplace Restrictions Approved Sources Datasheet Management
Request a Quotation from participating marketplace vendors Request Updated Every Day 2835-01-413-0217
Restrictions Approved Sources Datasheet Management https//www.nsnlookup.com /fsg-28/fsc-2835/us 2835-01-413-0217
2835014130217 014130217,501E123ED-P-63 Non-Aircraft Prime Mover, Aircraft Non-Prime Mover, and
Every Day 2835-01-389-2867 RQST NE Restrictions https//www.nsnlookup.com /fsg-28/fsc-2835/us 2835-01-413-0217
2835014130217 014130217,501E123ED-P-63 web browser . 2835-01-413-0217Nonaircraft Gas Turbine Engine
Turbine Rotor2835014130217 014130217 501E123ED-P Restrictions 2835-01-389-2867 DEMIL: A | DEMILI : |
1995 2835-01-413-3909 Lever Pump Assembly 1386AS186-1RNCC: 3 | RNVC: 2 | DAC: 1 12 May 1995 2835-01-413-0217

2835-01-413-0217 Demil Restrictions 2835-01-413-0217

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

2835-01-413-0217 is a Nonaircraft 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 is considered a low risk when released from the control of the Department of Defense. The item may still be subject to the requirements of the Export Administration Regulations (EAR) and the Code of Federal Regulations (CFR). This item is not suspected to be hazardous. This item does not contain a precious metal.

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