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2840-00-970-8921

Aircraft Gas Turbine Engine Turbine Nozzle

2840009708921 009708921 1-140-270-13

A single 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. View more Aircraft Gas Turbine Engine Turbine Nozzle

2840-00-970-8921 NOZZLE,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840009708921 009708921

Managed by United States
NSN Created on 1 Jan 1962
Data Last Changed
November 2023
NATO Update Count
12
NATO Data Quality
2840-00-970-8921 NOZZLE,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840009708921 009708921 1/1
NSN 2840-00-970-8921 (Generic Image) 1/1

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2840-00-970-8921 Related Documents Related Documents 2840-00-970-8921 2+ Documents (More...)

2840-00-948-5123 2840009485123 009485123 is a single 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.
7757 Aircraft Gas Turbine Engine Turbine Nozzle 477251CL11RNCC: 3 | RNVC: 2 | DAC: 2 1 Jan 1962 2840-00-970-8921

2840-00-970-8921 Demil Restrictions 2840-00-970-8921

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

2840-00-970-8921 is a Aircraft Gas Turbine Engine Turbine Nozzle 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. The precious metals content of this item is unknown.

2840-00-970-8921 Manufacturers Approved Sources 2840-00-970-8921

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