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2840-01-350-8509
Aircraft Gas Turbine Engine Component Mounting Plate
2840013508509 013508509 3661437-5
A metallic item of various shapes designed to reduce vibration and to secure a component part of an ENGINE, GAS TURBINE, AIRCRAFT to the engine case or housing as modified. For mounting accessories to the outside of the engine, see PLATE, MOUNTING. View more Aircraft Gas Turbine Engine Component Mounting Plate
January 2023
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Restrictions 2840-01-350-8509
2840-01-350-8509 is a Aircraft Gas Turbine Engine Component Mounting Plate 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 2840-01-350-8509
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 2840-01-350-8509
- Taiwan, Province of China (YE01)
- Effective Date:
- 1 Feb 2015
Approved Sources 2840-01-350-8509
- Part Number
- Manufacturer
- Status
- 3661437-5
- Manufacturer
- 99193 - Honeywell International Inc. (Active)
- Primary Buy
- Primary Buy
Datasheet 2840-01-350-8509
- Characteristic
- Specifications
- FIIG
- Specifications
- A530F0
- End Item Identification [AGAV]
- Pacer Dawn
- Criticality Code Justification [CRTL]
- Agav
- Diameter [ABMZ]
- 7.720 Inches Minimum And 7.780 Inches Maximum
- Engine Section Location [CZBJ]
- Compressor
- Material [MATT]
- Steel Corrosion Resisting Overall
- Overall Length [ABHP]
- 0.835 Inches Nominal
NATO Stock Numbers Related to 2840-01-350-8509
Freight Information 2840-01-350-8509
2840-01-350-8509 has freight characteristics managed by the Department of Energy (DOE).. 2840-01-350-8509 has a variance between NMFC and UFC when transported by rail and the description should be consulted.