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1560-01-515-8577
Aircraft Structural Component Fitting
1560015158577 015158577 5HF43775-109
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
3

Marketplace 1560-01-515-8577
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Related Documents 1560-01-515-8577 2+ Documents (More...)
United States (US) 4. 1560-01-515-8577 Marketplace Restrictions Approved Sources Datasheet Management
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Restrictions 1560-01-515-8577
1560-01-515-8577 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. The DCMO has forced the Demilization requirements for this item as the ICP has not collaborated. 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 1560-01-515-8577
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 1560-01-515-8577
- US Air Force (FLL5)
- Effective Date:
- 1 Dec 2003
Approved Sources 1560-01-515-8577
- Part Number
- Manufacturer
- Status
- 5HF43775-109
- Manufacturer
- 81755 - Lockheed Martin Corporation (Active)
- Primary Buy
- Primary Buy
Datasheet 1560-01-515-8577
- Characteristic
- Specifications
- FIIG
- Specifications
- A11800
- End Item Identification [AGAV]
- F-22A Raptor
- Aircraft Location [CZDJ]
- Fitting, Aim 120 Launcher
- Aircraft Mission Design Series [CZEK]
- F-22A
- Material Thickness [ABPX]
- 1.750 Nominal Inches
- Material [MATT]
- Titanium Alloy
- Overall Length [ABHP]
- 3.166 Inches Nominal
- Overall Width [ABMK]
- 2.000 Inches Nominal
- Part Name Assigned By Controlling Agency [CXCY]
- Fitting Assembly
- Special Features [FEAT]
- Fracture/Durability Critical Item, Cat 2; Dim Are Stock Material; M/F: 6Al-4V Eli Titanium Beta Ann Plate; C/O: -101 Fitting & Ft1761-12Pt Ring(4)
Management Data 1560-01-515-8577
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Freight Information 1560-01-515-8577
1560-01-515-8577 has freight characteristics.. 1560-01-515-8577 has a variance between NMFC and UFC when transported by rail and the description should be consulted.