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1560-01-488-0237
Aircraft Structural Component Support
1560014880237 014880237 5HH44517-167
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
3
Marketplace 1560-01-488-0237
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Related Documents 1560-01-488-0237 1+ Documents (More...)
United States (US) 4. 1560-01-488-0237 Marketplace Restrictions Approved Sources Datasheet Management
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Restrictions 1560-01-488-0237
1560-01-488-0237 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 1560-01-488-0237
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 1560-01-488-0237
- US Air Force (FLL5)
- Effective Date:
- 1 Aug 2001
Approved Sources 1560-01-488-0237
- Part Number
- Manufacturer
- Status
- 5HH44517-167
- Manufacturer
- 81755 - Lockheed Martin Corporation (Active)
- Primary Buy
- Primary Buy
Datasheet 1560-01-488-0237
- Characteristic
- Specifications
- FIIG
- Specifications
- A11800
- End Item Identification [AGAV]
- F-22 Raptor
- Aircraft Mission Design Series [CZEK]
- F-22 Raptor
- Material Document And Classification [MDCL]
- Qq-A-250/4 Assn Std All Material Responses
- Material Thickness [ABPX]
- 0.125 Inches Maximum
- Material [MATT]
- Aluminum Alloy 2024
- Overall Length [ABHP]
- 4.000 Inches Maximum
- Overall Width [ABMK]
- 2.000 Inches Maximum
- Part Name Assigned By Controlling Agency [CXCY]
- Support Assembly
- Special Features [FEAT]
- Consists Of 1 5Hh44517-169 Support; 2 Lk204f3 Nuts And 4 Ms20426ad3-4 Rivets
Management Data 1560-01-488-0237
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Freight Information 1560-01-488-0237
1560-01-488-0237 has freight characteristics.. 1560-01-488-0237 has a variance between NMFC and UFC when transported by rail and the description should be consulted.