2840-37-522-3531

Aircraft Gas Turbine Engine Combustion Chamber

2840375223531 375223531 KDC 2835-T4002 A80611120 A80611120-01

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

Managed by Korea

NSN Created on 21 Dec 2011

Data Last Changed
January 2023

NATO Update Count
1

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2840-37-522-3531 CHAMBER,COMBUSTION,AIRCRAFT GAS TURBINE ENGINE 2840375223531 375223531 1/1 — NSN 2840-37-522-3531 (Generic Image) 1/1

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KDC 2835-T4002 A80611120 A80611120-01 The portion of an ENGINE, GAS TURBINE, AIRCRAFT in which fuel
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Restrictions 2840-37-522-3531

2840-37-522-3531 is a Aircraft Gas Turbine Engine Combustion Chamber

End Users 2840-37-522-3531

Republic of Korea (ZH)

Approved Sources 2840-37-522-3531

Part Number
Manufacturer
Status
KDC 2835-T4002: 3999F - Defense Acquisition Program (Active); Related Standard; RNCC 2 RNVC 1 DAC 3
A80611120: 3999F - Defense Acquisition Program (Active); Primary Buy; RNCC 3 RNVC 2 DAC 1
A80611120-01: 3999F - Defense Acquisition Program (Active); Primary Buy; RNCC 3 RNVC 2 DAC 3
A80611120-01: 1645F - Hanwha Aerospace Co., Ltd (Active); Secondary Buy; RNCC 5 RNVC 2 DAC 3

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