2840-14-471-4553

Aircraft Gas Turbine Engine Combustion Chamber

2840144714553 144714553 304-825-413-0

The portion of an ENGINE, GAS TURBINE, AIRCRAFT in which fuel is burned. It may be an annular type in which the space between the circular inner and outer cylinders form the burning chamber or it may be the multi-arrangement can type in which separate can like burn cylinders are positioned in a circular arrangement within an inner and outer case. View more Aircraft Gas Turbine Engine Combustion Chamber

2840-14-471-4553 CHAMBER,COMBUSTION,AIRCRAFT GAS TURBINE ENGINE 2840144714553 144714553

Managed by France
NSN Created on 29 Aug 1994
Data Last Changed
January 2023
NATO Update Count
1
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2840-14-471-4553 Related Documents Related Documents 2840-14-471-4553 3+ Documents (More...)

827-2632 Part NumberManufacturerStatusFV 825413 https//www.nsnlookup.com /fsg-28/fsc-2840/fr 2840-14-471-4553
2840144714553 144714553,304-825-413-0 2840-14-471-4553 2840144714553 144714553 is the portion of
2840-99-361-4421 2840993614421 993614421 is the portion of an engine, gas turbine, aircraft in which fuel is burned. it may be an annular type in which the space between the circular inner and outer cylinders form the burning chamber or it may be the multi-arrangement can type in which separate can like burn cylinders are positioned in a circular arrangement within an inner and outer case.
6042 Aircraft Gas Turbine Engine Combustion Chamber 697197RNCC: 3 | RNVC: 2 | DAC: 6 4 Feb 1975 2840-14-471-4553

2840-14-471-4553 Demil Restrictions 2840-14-471-4553

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

2840-14-471-4553 is a Aircraft Gas Turbine Engine Combustion Chamber

2840-14-471-4553 End Users End Users 2840-14-471-4553

France (ZF)
Greece (ZU)

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