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2840-01-471-2558
Aircraft Gas Turbine Engine Combustion Chamber Duct
2840014712558 014712558 7-W11670023-23
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
January 2023
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United States (US) 4. 2840-01-471-2558 Marketplace Restrictions Approved Sources Datasheet Management
RQST NE Updated Every Day 2840-01-471-2558 RQST Updated Every Day 2840-01-471-2558 RQST NE Related Documents
Restrictions 2840-01-471-2558
2840-01-471-2558 is a Aircraft Gas Turbine Engine Combustion Chamber Duct that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. Demilitarization of this item has been confirmed and is not currently subject to changes. This item is considered a low risk when released from the control of the Department of Defense. The item may still be subject to the requirements of the Export Administration Regulations (EAR) and the Code of Federal Regulations (CFR). This item is not suspected to be hazardous. This item does not contain a precious metal.
Import and Export 2840-01-471-2558
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 2840-01-471-2558
- United Kingdom (ZK01)
- Effective Date:
- 1 Jan 2000
Approved Sources 2840-01-471-2558
- Part Number
- Manufacturer
- Status
- 7-W11670023-23
- Manufacturer
- 8V613 - The Boeing Company (Active)
- Primary Buy
- Primary Buy
Datasheet 2840-01-471-2558
- Characteristic
- Specifications
- FIIG
- Specifications
- A530F0
- End Item Identification [AGAV]
- Used On Mcdonnell Douglas Ah-64 Apache Helicopter
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Freight Information 2840-01-471-2558
2840-01-471-2558 has freight characteristics managed by the Bureau of Engraving and Printing.. 2840-01-471-2558 has a variance between NMFC and UFC when transported by rail and the description should be consulted.