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1560-01-488-1331
Aircraft Structural Component Fitting
1560014881331 014881331 5HA49220-103
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
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May 2023
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Related Documents 1560-01-488-1331 1+ Documents (More...)
United States (US) 4. 1560-01-488-1331 Marketplace Restrictions Approved Sources Datasheet Management
/fsc-1560/us 1560-01-488-1331 Aircraft Structural Component Fitting 5HA49220-103 An item of unique shapes
Restrictions 1560-01-488-1331
1560-01-488-1331 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 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 1560-01-488-1331
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 1560-01-488-1331
- US Air Force (FLL5)
- Effective Date:
- 1 Aug 2001
Approved Sources 1560-01-488-1331
- Part Number
- Manufacturer
- Status
- 5HA49220-103
- Manufacturer
- 81755 - Lockheed Martin Corporation (Active)
- Primary Buy
- Primary Buy
Datasheet 1560-01-488-1331
- Characteristic
- Specifications
- FIIG
- Specifications
- A11800
- End Item Identification [AGAV]
- F-22 Raptor
- Aircraft Location [CZDJ]
- Aft Outboard Door Interface
- Aircraft Mission Design Series [CZEK]
- F-22A
- Material [MATT]
- Aluminum Alloy 2124
- Overall Length [ABHP]
- 8.000 Inches Nominal
- Overall Width [ABMK]
- 3.000 Inches Nominal
- Part Name Assigned By Controlling Agency [CXCY]
- Fitting, Assembly Of
- Special Features [FEAT]
- Dim. Are Stock Material; C/O: -101 Fitting & Nas77a4-010 Bushing (2); M/O: 2124-T8151 Aluminum Plate
Management Data 1560-01-488-1331
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Freight Information 1560-01-488-1331
1560-01-488-1331 has freight characteristics.. 1560-01-488-1331 has a variance between NMFC and UFC when transported by rail and the description should be consulted.