Premium Information is available for this item - Upgrade for $1 a day
1560-01-488-5357
Aircraft Structural Component Bracket
1560014885357 014885357 5HF71455-193
An item of various configuration that is an integral member of the airframe structure. It is specifically designed for the purpose of maintaining, positioning, joining, and strengthening the aircraft structure. It may include holes for mounting purposes or to form an assembly. View more Aircraft Structural Component Bracket
![]()
May 2023
4

Marketplace 1560-01-488-5357
Request a Quotation from participating marketplace vendors
Related Documents 1560-01-488-5357 1+ Documents (More...)
United States (US) 4. 1560-01-488-5357 Marketplace Restrictions Approved Sources Datasheet Management
Request a Quotation from participating marketplace vendors Request Updated Every Day 1560-01-488-5357
Restrictions 1560-01-488-5357
1560-01-488-5357 is a Aircraft Structural Component Bracket 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 1560-01-488-5357
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 1560-01-488-5357
- US Air Force (FLL5)
- Effective Date:
- 1 Aug 2001
Approved Sources 1560-01-488-5357
- Part Number
- Manufacturer
- Status
- 5HF71455-193
- Manufacturer
- 81205 - The Boeing Company (Active)
- Primary Buy
- Primary Buy
Datasheet 1560-01-488-5357
- Characteristic
- Specifications
- FIIG
- Specifications
- A11800
- End Item Identification [AGAV]
- F/A-22 Raptor
- Aircraft Location [CZDJ]
- Upper Skin, Rework
- Aircraft Mission Design Series [CZEK]
- F/A-22 Raptor
- Material Document And Classification [MDCL]
- Mil-T-9046 Mil Spec Single Material Response
- Material Thickness [ABPX]
- 0.125 Inches Nominal
- Material [MATT]
- Titanium
- Overall Length [ABHP]
- 4.000 Inches Nominal
- Overall Width [ABMK]
- 1.000 Inches Nominal
- Part Name Assigned By Controlling Agency [CXCY]
- Clip
- Special Features [FEAT]
- Annealed Titanium Sheet
Management Data 1560-01-488-5357
Similar Supply Items to 1560-01-488-5357


















Freight Information 1560-01-488-5357
1560-01-488-5357 has freight characteristics.. 1560-01-488-5357 has a variance between NMFC and UFC when transported by rail and the description should be consulted.