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2840-01-347-2181
Aircraft Gas Turbine Engine Fan Case
2840013472181 013472181 3097233-2
A case that is an integral part of an ENGINE, GAS TURBINE, AIRCRAFT, designed to surround and protect a FAN, AIRCRAFT GAS TURBINE ENGINE. View more Aircraft Gas Turbine Engine Fan Case
January 2023
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Restrictions 2840-01-347-2181
2840-01-347-2181 is a Aircraft Gas Turbine Engine Fan Case 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 2840-01-347-2181
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 2840-01-347-2181
- Taiwan, Province of China (YE01)
- Effective Date:
- 1 Feb 2015
Approved Sources 2840-01-347-2181
- Part Number
- Manufacturer
- Status
- 3097233-2
- Manufacturer
- 99193 - Honeywell International Inc. (Active)
- Primary Buy
- Primary Buy
Datasheet 2840-01-347-2181
- Characteristic
- Specifications
- FIIG
- Specifications
- A10700
- End Item Identification [AGAV]
- Pacer Dawn
- Criticality Code Justification [CRTL]
- Agav
- Diameter [ABMZ]
- 20.621 Inches Minimum And 20.625 Inches Maximum
- Engine Section Location [CZBJ]
- Fan
- Material Thickness [ABPX]
- 0.060 Inches Minimum And 0.070 Inches Maximum
- Material [MATT]
- Steel Outer Case
- Special Features [FEAT]
- 3Rd Stage
- Overall Length [ABHP]
- 3.903 Inches Minimum And 3.909 Inches Maximum
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Freight Information 2840-01-347-2181
2840-01-347-2181 has freight characteristics managed by the Department of Energy (DOE).. 2840-01-347-2181 has a variance between NMFC and UFC when transported by rail and the description should be consulted.