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2840-01-538-9359
Aircraft Gas Turbine Engine Turbine Nozzle Assembly
2840015389359 015389359 3101513-17
A stationary item designed for the purpose of directing air at the proper angle and velocity to a ROTOR, TURBINE, AIRCRAFT GAS TURBINE ENGINE. It has provisions for attaching to a CASE (3), TURBINE, AIRCRAFT GAS TURBINE ENGINE. It may have an inner support shroud. The assembled item forms a complete circle. View more Aircraft Gas Turbine Engine Turbine Nozzle Assembly
May 2023
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Related Documents 2840-01-538-9359 1+ Documents (More...)
RQST NE Updated Every Day 2840-01-538-9359 RQST Updated Every Day 2840-01-538-9359 RQST NE Related Documents
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Restrictions 2840-01-538-9359
2840-01-538-9359 is a Aircraft Gas Turbine Engine Turbine Nozzle Assembly 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 2840-01-538-9359
- Schedule B
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- HTS Code
- Subscribe to View HTS Code
End Users 2840-01-538-9359
- Spain (YB01)
- Effective Date:
- 1 Apr 2006
Approved Sources 2840-01-538-9359
- Part Number
- Manufacturer
- Status
- 3101513-17
- Manufacturer
- 99193 - Honeywell International Inc. (Active)
- Primary Buy
- Primary Buy
Datasheet 2840-01-538-9359
- Characteristic
- Specifications
- FIIG
- Specifications
- A10700
- End Item Identification [AGAV]
- Aviocar C212
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Freight Information 2840-01-538-9359
2840-01-538-9359 has freight characteristics.. 2840-01-538-9359 has a variance between NMFC and UFC when transported by rail and the description should be consulted.