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1560-01-558-5366
Aircraft Structural Component Fitting
1560015585366 015585366 5HL71022-101
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
January 2023
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United States (US) 4. 1560-01-558-5366 Marketplace Restrictions Approved Sources Datasheet Management
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Restrictions 1560-01-558-5366
1560-01-558-5366 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 1560-01-558-5366
- Schedule B
- Subscribe to View Schedule B
- HTS Code
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End Users 1560-01-558-5366
- US Air Force (FLL5)
- Effective Date:
- 1 Nov 2007
Approved Sources 1560-01-558-5366
- Part Number
- Manufacturer
- Status
- 5HL71022-101
- Manufacturer
- 81205 - The Boeing Company (Active)
- Primary Buy
- Primary Buy
Datasheet 1560-01-558-5366
- Characteristic
- Specifications
- FIIG
- Specifications
- A11800
- End Item Identification [AGAV]
- F-22 Raptor Aircraft
- Aircraft Location [CZDJ]
- Uplock Strut,Arresting Gear
- Aircraft Mission Design Series [CZEK]
- F-22 Raptor Acft
- Material Document And Classification [MDCL]
- Mil-T-9047 Mil Spec Single Material Response
- Material [MATT]
- Titanium Alloy
- Overall Length [ABHP]
- 2.000 Inches Nominal
- Part Name Assigned By Controlling Agency [CXCY]
- Cylinder
- Special Features [FEAT]
- Ann Titanium Rod;Dim.Are Stocksize Matl
Management Data 1560-01-558-5366
- Effective Date
- Organization
- Unit of Issue
- Unit Price
- Qty Unit Pack
- Unit of Issue
- Nov 2007
- Department of the Air Force (DF)
- EA
- Subscribe
- 1
- EA
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Freight Information 1560-01-558-5366
1560-01-558-5366 has freight characteristics.. 1560-01-558-5366 has a variance between NMFC and UFC when transported by rail and the description should be consulted.