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2840-01-347-6915
Aircraft Gas Turbine Engine Diffuser
2840013476915 013476915 3092100-5
A frame with stationary struts, designed to diffuse and direct air from the COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE. It may have mounting facilities for external components. It may provide support and house a compressor rear bearing. May include a CASE (3), DIFFUSER, AIRCRAFT GAS TURBINE ENGINE. View more Aircraft Gas Turbine Engine Diffuser
January 2023
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Restrictions 2840-01-347-6915
2840-01-347-6915 is a Aircraft Gas Turbine Engine Diffuser 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 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 2840-01-347-6915
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 2840-01-347-6915
- Taiwan, Province of China (YE01)
- Effective Date:
- 1 Feb 2015
- Malaysia (YW01)
- Effective Date:
- 1 Aug 2007
Approved Sources 2840-01-347-6915
- Part Number
- Manufacturer
- Status
- 3092100-5
- Manufacturer
- 99193 - Honeywell International Inc. (Active)
- Primary Buy
- Primary Buy
Datasheet 2840-01-347-6915
- Characteristic
- Specifications
- FIIG
- Specifications
- A10700
- End Item Identification [AGAV]
- Pacer Dawn
- Criticality Code Justification [CRTL]
- Agav
- Engine Section Location [CZBJ]
- Diffuser
- Material [MATT]
- Nickel Alloy Overall
- Overall Length [ABHP]
- 5.490 Inches Minimum And 5.511 Inches Maximum
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Freight Information 2840-01-347-6915
2840-01-347-6915 has freight characteristics managed by the Department of Energy (DOE).. 2840-01-347-6915 has a variance between NMFC and UFC when transported by rail and the description should be consulted.