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1560-01-586-4787
Aircraft Structural Component Support
1560015864787 015864787 7-311113513-247 7-311113513
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
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Related Documents 1560-01-586-4787 5+ Documents (More...)
-107 7-311113513 An item of various configuration that is an integral member of the airframe structure
-149 7-311113513 A device of various shapes to be permanently attached to the structure of an aircraft
-321 7-311113513 An item, generally a strip, designed to strengthen and resist loads by attachment to
-107 7-311113513 An item of various configuration that is an integral member of the airframe structure
-49 7-311113513 A device of various shapes to be permanently attached to the structure of an aircraft
-107 7-311113513 An item of various configuration that is an integral member of the airframe structure
-135 7-311113513 A short, longitudinal member which joins adjacent frames, ribs, and the like.
- Upgrade for $1 a day Upgrade your Account Upgrade 5365-01-586-8871Shim5365015868871 015868871 7-311113513
-163 7-311113513 An item of various configuration that is an integral member of the airframe structure
-141 7-311113513 An item of various configuration that is an integral member of the airframe structure
Restrictions 1560-01-586-4787
1560-01-586-4787 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 has been confirmed as a Critical Munitions List Item or a Sensitive Commerce Control List Item and cannot be in the possession of any party anywhere in the World who is not an authorized NATO Government. Any other possessor of this item should mutilate it now as possession violates international and local laws. This item is a confirmed Commerce Control List Item (CCLI). 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 1560-01-586-4787
- Schedule B
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- HTS Code
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End Users 1560-01-586-4787
- US Army (A703)
- Effective Date:
- 1 Jun 2010
- United Kingdom (ZK01)
- Effective Date:
- 1 Oct 2010
Approved Sources 1560-01-586-4787
- Part Number
- Manufacturer
- Status
- 7-311113513-247
- Manufacturer
- 8V613 - The Boeing Company (Active)
- Primary Buy
- Primary Buy
- 7-311113513
- 8V613 - The Boeing Company (Active)
- Informational Drawing
- Informational Drawing
Management Data 1560-01-586-4787
Army
- Materiel Category and Inventory Manager:
- H
- Aircraft, Air Materiel
- Appropriation and Budget Activity:
- 2
- Stock Fund Secondary Items
- Management Inventory Segment:
- 2
- Non-Repairable Items(Exclusive of Insurance and Provisioning Items)
This code will be used to identify items, which are not reparable.
- Weapons System / End Item / Homogeneous Group:
- BJ
- Rotary Wing Aircraft
AH-64 Airframe
- Accounting Requirements:
- X
- Expendable item.An item of Army property coded with an ARC of X in the AMDF. Expendable items require no formal accountability after issue from a stock record account.Commercial and fabricated items similar to items coded X in the AMDF are considered expendable items.
NATO Stock Numbers Related to 1560-01-586-4787
Freight Information 1560-01-586-4787
1560-01-586-4787 has freight characteristics.. 1560-01-586-4787 has a variance between NMFC and UFC when transported by rail and the description should be consulted.