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2840-00-897-7230

Aircraft Gas Turbine Engine Combustion Chamber Duct

2840008977230 008977230 434299

A cylindrical shaped item or a segment thereof designed to direct air into or around a CHAMBER, COMBUSTION, AIRCRAFT GAS TURBINE ENGINE. The internal iar is divided and directed to the burning chamber(s). The external air is used for cooling purposes. View more Aircraft Gas Turbine Engine Combustion Chamber Duct

2840-00-897-7230 DUCT,COMBUSTION CHAMBER,AIRCRAFT GAS TURBINE ENGINE 2840008977230 008977230

Managed by United States
NSN Created on 1 Jan 1963
Data Last Changed
November 2023
NATO Update Count
12
NATO Data Quality
2840-00-897-7230 DUCT,COMBUSTION CHAMBER,AIRCRAFT GAS TURBINE ENGINE 2840008977230 008977230 1/1
NSN 2840-00-897-7230 (Generic Image) 1/1

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2840-00-897-7230 Related Documents Related Documents 2840-00-897-7230 5+ Documents (More...)

434299 A cylindrical shaped item or a segment thereof designed to direct air into or around a CHAMBER
United States (US) 4. 2840-00-897-7230 Marketplace Restrictions Approved Sources Datasheet Management
RQST NE Updated Every Day 2840-00-897-7230 RQST Updated Every Day 2840-00-897-7230 RQST NE Related
JavaScript in your web browser . 3120-14-502-9646Cam Follower Plain Bearing3120145029646 145029646 434299
434299-003 A detachable assembly, which provides rolling contact with a cam or similar device, and converts
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2840-00-897-7230 Demil Restrictions 2840-00-897-7230

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

2840-00-897-7230 is a Aircraft Gas Turbine Engine Combustion Chamber Duct 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.

2840-00-897-7230 Manufacturers Approved Sources 2840-00-897-7230

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