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1560-01-359-1047
Aircraft Structural Component Support
1560013591047 013591047 68A111211-2030
A device of various shapes to be permanently attached to the structure of an aircraft. It is designed to permanently mount and/or support an integral member, or group of members of the airframe in a proper position and bear the stress imposed by the components being supported. It may have mounting provisions, such as slots, holes, and/or attachments to facilitate installation. Excludes items which are primarily designed for dampening shock and/or vibration. Excludes BRACKET, ANGLE; BRACKET, DOUBLE ANGLE; BRACKET, SHELF; BRACKET, MOUNTING; BRACKET (1), STRUCTURAL COMPONENT, AIRCRAFT; and RADIUS BLOCK. View more Aircraft Structural Component Support
November 2023
6
Marketplace 1560-01-359-1047
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Related Documents 1560-01-359-1047 1+ Documents (More...)
United States (US) 4. 1560-01-359-1047 Marketplace Restrictions Approved Sources Datasheet Management
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Restrictions 1560-01-359-1047
1560-01-359-1047 is a Aircraft Structural Component Support that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. This item is a US Munitions List Item and must be mutilated to scrap. 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.
Approved Sources 1560-01-359-1047
- Part Number
- Manufacturer
- Status
- 68A111211-2030
- Manufacturer
- 76301 - The Boeing Company (Active)
- Primary Buy
- Primary Buy
Management Data 1560-01-359-1047
- Effective Date
- Organization
- Unit of Issue
- Unit Price
- Qty Unit Pack
- Unit of Issue
- Jun 2014
- Department of the Air Force (DF)
- EA
- Subscribe
- 1
- EA
- MOE
- USC
- Code
- Statement
- Order of Use
- Jump To Code
- Qty Per Assy
- UOM
- Technical Document
- Quantative Expression
- Code
- Department of the Air Force (DF)
- I
- V
- Discontinued Without Replacement
- V
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