2840-14-321-8518

Aircraft Gas Turbine Engine Combustion Chamber

2840143218518 143218518 RK32764AM0D1147 HE800-4477

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

2840-14-321-8518 CHAMBER,COMBUSTION,AIRCRAFT GAS TURBINE ENGINE 2840143218518 143218518

Managed by France
NSN Created on 1 Jan 1975
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
2840-14-321-8518 CHAMBER,COMBUSTION,AIRCRAFT GAS TURBINE ENGINE 2840143218518 143218518 1/1
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2840-14-321-8518 2840143218518 143218518,RK32764AM0D1147
RK32764AM0D1147 HE800-4477 The portion of an ENGINE, GAS TURBINE, AIRCRAFT in which fuel is burned.
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2840-14-321-8518 Demil Restrictions 2840-14-321-8518

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2840-14-321-8518 is a Aircraft Gas Turbine Engine Combustion Chamber

2840-14-321-8518 End Users End Users 2840-14-321-8518

France (ZF)

2840-14-321-8518 Manufacturers Approved Sources 2840-14-321-8518

Part Number
Manufacturer
Status
HE800-4477
F5385 - Section De Codification 85 (Cancelled)
Primary Buy
RNCC 3 RNVC 2 DAC 6
RK32764AM0D1147
K0680 - Rolls-Royce Airlines (Active)
Incomplete Secondary Reference
RNCC 5 RNVC 1 DAC 6

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