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1560-01-466-7375
Aircraft Structural Component Fitting
1560014667375 014667375 7-511180014-5
An item of unique shapes and cross-sectional configurations specifically designed with dimensional tolerances and finishes. It may be metallic and/or nonmetallic and must be able to mate with or join to like items with aircraft application. The item may consist of more then one (1) piece to form an assembly. Do not use if a more specific item name exists. Excludes BRACKET (1), STRUCTURAL COMPONENT, AIRCRAFT. View more Aircraft Structural Component Fitting
May 2023
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Restrictions 1560-01-466-7375
1560-01-466-7375 is a Aircraft Structural Component Fitting 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 may be hazardous as it is in a Federal Supply Class for potentially hazardous items. A MSDS should be available from the supplier for the end user to evaluate any hazards. This item does not contain a precious metal.
Import and Export 1560-01-466-7375
- Schedule B
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- HTS Code
- Subscribe to View HTS Code
End Users 1560-01-466-7375
- United Kingdom (ZK01)
- Effective Date:
- 1 Jul 1999
Approved Sources 1560-01-466-7375
- Part Number
- Manufacturer
- Status
- 7-511180014-5
- Manufacturer
- 8V613 - The Boeing Company (Active)
- Primary Buy
- Primary Buy
Datasheet 1560-01-466-7375
- Characteristic
- Specifications
- FIIG
- Specifications
- A11800
- End Item Identification [AGAV]
- Aphace Ah-64D Helicopter
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Freight Information 1560-01-466-7375
1560-01-466-7375 has freight characteristics managed by the Bureau of Engraving and Printing.. 1560-01-466-7375 has a variance between NMFC and UFC when transported by rail and the description should be consulted.