2840-25-142-1989

Aircraft Gas Turbine Engine Combustion Chamber Liner

2840251421989 251421989

A cylindrical shaped item positioned inside the CHAMBER, COMBUSTION, AIRCRAFT GAS TURBINE ENGINE. It is designed to direct the flow of hot gasses to the TURBINE ASSEMBLY, AIRCRAFT GAS TURBINE ENGINE. View more Aircraft Gas Turbine Engine Combustion Chamber Liner

2840-25-142-1989 LINER,COMBUSTION CHAMBER,AIRCRAFT GAS TURBINE ENGINE 2840251421989 251421989

Managed by Norway
Data Last Changed
January 2024
NATO Update Count
1
NATO Data Quality
2840-25-142-1989 LINER,COMBUSTION CHAMBER,AIRCRAFT GAS TURBINE ENGINE 2840251421989 251421989 1/1
NSN 2840-25-142-1989 (Generic Image) 1/1

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web browser . 2840-25-142-1989Aircraft Gas Turbine Engine Combustion Chamber Liner2840251421989 251421989
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www.nsnlookup.com /fsg-28/fsc-2840/no 2840-25-152-0503 Aircraft Gas Turbine Engine Turbine Rotor 25-142-1989 2840251421989
251421989 , Aircraft, Prime Moving; and Components from Norway (NO) 2840-25-118-2671 Moving; and Components
Machine Bolt 2840-25-118-2815 Bolt 2840-25-118-2671 https//www.nsnlookup.com /fsg-28/fsc-2840/no 2840-25-142-1989
-25-118-2671 Preformed Packing 2840-25-152-0503 https//www.nsnlookup.com /fsg-28/fsc-2840/no 2840-25-142-1989
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/fsg-28/fsc-2840/no 2840-25-152-0503 www.nsnlookup.com /fsg-28/fsc-2840/no 2840-25-142-1989 https//www.nsnlookup.com
Engines, Aircraft, Prime Moving; and Components from Norway (NO) Turbine Engine Turbine Rotor 2840-25-142-1989
2840-25-118-2671 Preformed Packing 2840-25-152-0503 Aircraft Gas Turbine Engine Turbine Rotor 2840-25-142-1989

2840-25-142-1989 Demil Restrictions 2840-25-142-1989

DEMIL: | DEMILI: | CRITICALITY: | HMIC: | PMIC: | EDC: | ADPEC:

2840-25-142-1989 is a Aircraft Gas Turbine Engine Combustion Chamber Liner

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