2835-01-440-2134

Nonaircraft Gas Turbine Engine Turbine Nozzle Assembly

2835014402134 014402134 107689-2

A stationary item designed for the purpose of directing air at the proper angle and velocity to a ROTOR, TURBINE, NONAIRCRAFT GAS TURBINE ENGINE. It has provisions for attaching to a CASE (3), TURBINE, NONAIRCRAFT GAS TURBINE ENGINE. It may have an inner support shroud. The assembled item forms a complete circle. View more Nonaircraft Gas Turbine Engine Turbine Nozzle Assembly

2835-01-440-2134 NOZZLE ASSEMBLY,TURBINE,NONAIRCRAFT GAS TURBINE ENGINE 2835014402134 014402134

Managed by United States
NSN Created on 7 Jan 1997
Data Last Changed
November 2023
NATO Update Count
3
NATO Data Quality
2835-01-440-2134 NOZZLE ASSEMBLY,TURBINE,NONAIRCRAFT GAS TURBINE ENGINE 2835014402134 014402134 1/1
NSN 2835-01-440-2134 (Generic Image) 1/1

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2835014402134 014402134,107689-2 554-0031 2950145540031 145540031 515-5281 2835-01-679-7171 2835
2835014402134 014402134,107689-2 2835-15-207-8400 2835-00-004-2632 2835-01-440-2134 https//www.nsnlookup.com
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-0031 2835-15-207-8400 https//www.nsnlookup.com https//www.nsnlookup.com /fsg-28/fsc-2835/us 2835-01-440-2134
: | CRITICALITY : | HMIC : N | PMIC : A | EDC: https//www.nsnlookup.com /fsg-28/fsc-2835/us 2835-01-440-2134
2835014402134 014402134,107689-2 2835-15-207-8400 2835-00-004-2632 2835-01-440-2134 https//www.nsnlookup.com
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2835014402134 014402134,107689-2 000042623,111R545G7 515-5281 2835-01-679-7171 2835-01-631-7383
2950-14-554-0031 2835-15-207-8400 2835-00-004-2632 2835-01-440-2134 https//www.nsnlookup.com /fsg-28
145540031 958-6994 2835-01-618-2411 2835-01-676 https//www.nsnlookup.com /fsg-28/fsc-2835/us 2835-01-440-2134
2835014402134 014402134,107689-2 2835-15-207-8400 2835-00-004-2632 2835-01-440-2134 https//www.nsnlookup.com
515-5281 2835-01-679-7171 2835-01-631-7383 2950-14-554-0031 2835-15-207-8400 2835-00-004-2632 2835-01-440-2134

2835-01-440-2134 Demil Restrictions 2835-01-440-2134

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

2835-01-440-2134 is a Nonaircraft Gas Turbine Engine Turbine Nozzle Assembly 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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