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1560-01-185-3809
Aircraft Structural Component Bracket
1560011853809 011853809 16K0548-15 16K0548-9
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
January 2023
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Related Documents 1560-01-185-3809 3+ Documents (More...)
United States (US) 4. 1560-01-185-3809 Marketplace Restrictions Approved Sources Datasheet Management
RQST NE Updated Every Day 1560-01-185-3809 RQST Updated Every Day 1560-01-185-3809 RQST NE Related Documents
16K0548-9 1560PL0659896 An item of various configuration that is an integral member of the airframe
Bracket your Account Upgrade 1560-01-185-3809Aircraft Structural Component Bracket1560011853809 011853809
Restrictions 1560-01-185-3809
1560-01-185-3809 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. This item is a US Munitions List Item and must be mutilated to scrap. 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 1560-01-185-3809
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 1560-01-185-3809
- Israel (YD01)
- Effective Date:
- 1 Apr 1991
- Republic of Korea (ZH01)
- Effective Date:
- 1 Apr 1991
Approved Sources 1560-01-185-3809
- Part Number
- Manufacturer
- Status
- 16K0548-15
- Manufacturer
- 81755 - Lockheed Martin Corporation (Active)
- Primary Buy
- Primary Buy
- 16K0548-9
- 81755 - Lockheed Martin Corporation (Active)
- Canceled/Obsolete
- Canceled/Obsolete
Datasheet 1560-01-185-3809
- Characteristic
- Specifications
- FIIG
- Specifications
- A11800
- Aircraft Location [CZDJ]
- Fwd Fuselage
- Aircraft Mission Design Series [CZEK]
- F-16
- Height [HGTH]
- 2.750 Inches Nominal
- Material [MATT]
- Aluminum Alloy
- Material Document And Classification [MDCL]
- Ams4218-T6 Fed Spec Single Material Response
- Overall Length [ABHP]
- 14.510 Inches Nominal
- Overall Width [ABMK]
- 0.500 Inches Nominal
- Special Features [FEAT]
- Canopy Mounted Body Positioning Hfeatgandle
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Freight Information 1560-01-185-3809
1560-01-185-3809 has freight characteristics.. 1560-01-185-3809 has a variance between NMFC and UFC when transported by rail and the description should be consulted.