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1560-01-488-1663
Aircraft Structural Component Fitting
1560014881663 014881663 5HF43762-105
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
May 2023
5
Marketplace 1560-01-488-1663
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Related Documents 1560-01-488-1663 2+ Documents (More...)
United States (US) 4. 1560-01-488-1663 Marketplace Restrictions Approved Sources Datasheet Management
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Agency [CXCY]FittingSpecial Features [FEAT]Matt Is 2124 - T8151 Aluminum 3.000 Plate; Opposite 1560-01-488-1663
Restrictions 1560-01-488-1663
1560-01-488-1663 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 1560-01-488-1663
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 1560-01-488-1663
- US Air Force (FLL5)
- Effective Date:
- 1 Aug 2001
Approved Sources 1560-01-488-1663
- Part Number
- Manufacturer
- Status
- 5HF43762-105
- Manufacturer
- 81755 - Lockheed Martin Corporation (Active)
- Primary Buy
- Primary Buy
Datasheet 1560-01-488-1663
- Characteristic
- Specifications
- FIIG
- Specifications
- A11800
- End Item Identification [AGAV]
- F-22 Raptor
- Aircraft Location [CZDJ]
- Swb Pwr Hinge Lwr Lh/Rh
- Aircraft Mission Design Series [CZEK]
- F-22A
- Aircraft Station Number [CZEJ]
- Fs570.9
- Material Thickness [ABPX]
- 3.000 Nominal Inches
- Material [MATT]
- Aluminum Alloy 2124
- Overall Length [ABHP]
- 7.000 Inches Nominal
- Overall Width [ABMK]
- 5.000 Inches Nominal
- Part Name Assigned By Controlling Agency [CXCY]
- Fitting
- Special Features [FEAT]
- Dims. Are Stock Material; M/F 2124-T8151 Aluminum Plate
Management Data 1560-01-488-1663
- Effective Date
- Organization
- Unit of Issue
- Unit Price
- Qty Unit Pack
- Unit of Issue
- Nov 2022
- Department of the Air Force (DF)
- EA
- Subscribe
- 1
- EA
- May 2018
- 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)
- F
- F
- When Exhausted Use 1560-01-501-7314
- F
- Department of the Air Force (DF)
- I
- F
- When Exhausted Use 1560-01-501-7314
- F
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Freight Information 1560-01-488-1663
1560-01-488-1663 has freight characteristics.. 1560-01-488-1663 has a variance between NMFC and UFC when transported by rail and the description should be consulted.