2840-01-188-3771

Aircraft Gas Turbine Engine Turbine Nozzle Assembly

2840011883771 011883771 2184251CL13

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

2840-01-188-3771 NOZZLE ASSEMBLY,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840011883771 011883771

Managed by United States
NSN Created on 2 Sep 1984
Data Last Changed
November 2023
NATO Update Count
11
NATO Data Quality
2840-01-188-3771 NOZZLE ASSEMBLY,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840011883771 011883771 1/1
NSN 2840-01-188-3771 (Generic Image) 1/1

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2840-01-188-3771 Related Documents Related Documents 2840-01-188-3771 3+ Documents (More...)

5 17 Nov 2000 5365-01-480-5886 Bushing Blank 785016CL1RNCC: 3 | RNVC: 2 | DAC: 5 28 Nov 2000 2840-01-188-3771
Aircraft Gas Turbine Engine Turbine Nozzle Assembly 2184051CL3RNCC: 3 | RNVC: 2 | DAC: 4 2 Sep 1984 2840-01-188-3771
2840-01-188-3765 2840011883765 011883765 is 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.

2840-01-188-3771 Demil Restrictions 2840-01-188-3771

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

2840-01-188-3771 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 a US Munitions List Item and must be mutilated to scrap. This item is not suspected to be hazardous. This item does not contain a precious metal.

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