2840-01-441-0109

Aircraft Gas Turbine Engine Turbine Nozzle Assembly

2840014410109 014410109 4083403

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

2840-01-441-0109 NOZZLE ASSEMBLY,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840014410109 014410109

Managed by United States
NSN Created on 30 Jan 1997
Data Last Changed
November 2023
NATO Update Count
2
NATO Data Quality
2840-01-441-0109 NOZZLE ASSEMBLY,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840014410109 014410109 1/1
NSN 2840-01-441-0109 (Generic Image) 1/1

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2840-01-441-0109 Related Documents Related Documents 2840-01-441-0109 5+ Documents (More...)

| RNVC: 9 | DAC: 2 28 May 1997 2840-01-444-6990 https//www.nsnlookup.com /fsg-28/fsc-2840/us 2840-01-441-0109
2840014410109 014410109,4083403 2840-01-441-0109 2840014410109 014410109 is a stationary item designed
5950-01-408-3403 5950014083403 014083403 is a transformer consisting of one or more primary winding(s) and one or more secondary winding(s). it may be designed for direct connection to an alternating current source for purposes of changing the secondary volts and amperes or designed to eliminate metallic interconnection between circuits in an overall one to one voltage ratio, with or without additional output windings, or items designed to automatically maintain a constant output voltage within specified limits under varying input or load conditions. also includes items having a provision for mechanically changing the turns ratio or inductive coupling in progressive increments by means of voltage taps, ratio adjuster, or devices oe similar design. for transformers having winding(s) common to both input and output circuits, see transformer (1), power, autotransformer. excludes transformer (1), pulse.
Gas Turbine Engine Turbine Nozzle Assembly 1881M31G02RNCC: 3 | RNVC: 2 | DAC: 2 14 May 1997 2840-01-441-0109

2840-01-441-0109 Demil Restrictions 2840-01-441-0109

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

2840-01-441-0109 is a Aircraft Gas Turbine Engine Turbine Nozzle Assembly that does not have a nuclear hardened feature, but does have another critical feature or features 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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