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1560-01-542-9862
Aircraft Structural Component Support
1560015429862 015429862 4323145
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
May 2023
2
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Related Documents 1560-01-542-9862 2+ Documents (More...)
United States (US) 4. 1560-01-542-9862 Marketplace Restrictions Approved Sources Datasheet Management
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(Active) Related Standard RNCC 2 RNVC 1 DAC 3 4323145 T5804 - Merve Otomotiv-Senol Yazici (Active) Related
Restrictions 1560-01-542-9862
1560-01-542-9862 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. Demilitarization of this item has been confirmed and is not currently subject to changes. This item is a US Munitions List or Commerce Control List Item which must be destroyed to prevent restoration or repair. Only authorized parties may possess this item. 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 1560-01-542-9862
- Schedule B
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- HTS Code
- Subscribe to View HTS Code
End Users 1560-01-542-9862
- US Air Force (FLL5)
- Effective Date:
- 1 Aug 2006
Approved Sources 1560-01-542-9862
- Part Number
- Manufacturer
- Status
- 4323145
- Manufacturer
- 77445 - Rtx Corporation (Active)
- Primary Buy
- Primary Buy
Datasheet 1560-01-542-9862
- Characteristic
- Specifications
- FIIG
- Specifications
- A11800
- Aircraft Location [CZDJ]
- Te Plug,Closeout Plug
- Aircraft Mission Design Series [CZEK]
- F-22A
- Material [MATT]
- Titanium Alloy
- Overall Length [ABHP]
- 3.500 Inches Nominal
- Part Name Assigned By Controlling Agency [CXCY]
- Plug
- Special Features [FEAT]
- Closeout Plug,Matl Ams 4975 Titanium Alloy,Dim Are Stock Matl
Management Data 1560-01-542-9862
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Freight Information 1560-01-542-9862
1560-01-542-9862 has freight characteristics.. 1560-01-542-9862 has a variance between NMFC and UFC when transported by rail and the description should be consulted.