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1560-01-433-5200
Aircraft Structural Component Support
1560014335200 014335200 371412-1
A device of various shapes to be permanently attached to the structure of an aircraft. It is designed to permanently mount and/or support an integral member, or group of members of the airframe in a proper position and bear the stress imposed by the components being supported. It may have mounting provisions, such as slots, holes, and/or attachments to facilitate installation. Excludes items which are primarily designed for dampening shock and/or vibration. Excludes BRACKET, ANGLE; BRACKET, DOUBLE ANGLE; BRACKET, SHELF; BRACKET, MOUNTING; BRACKET (1), STRUCTURAL COMPONENT, AIRCRAFT; and RADIUS BLOCK. View more Aircraft Structural Component Support
January 2023
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Restrictions 1560-01-433-5200
1560-01-433-5200 is a Aircraft Structural Component Support that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. This item is considered a low risk when released from the control of the Department of Defense. The item may still be subject to the requirements of the Export Administration Regulations (EAR) and the Code of Federal Regulations (CFR). 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 1560-01-433-5200
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 1560-01-433-5200
- Poland (WP01)
- Effective Date:
- 1 Aug 2011
- United Kingdom (ZK01)
- Effective Date:
- 1 Jul 1996
Approved Sources 1560-01-433-5200
- Part Number
- Manufacturer
- Status
- 371412-1
- Manufacturer
- 98897 - Lockheed Martin Corp (Active)
- Primary Buy
- Primary Buy
Datasheet 1560-01-433-5200
- Characteristic
- Specifications
- FIIG
- Specifications
- A11800
- Material [MATT]
- Aluminum Alloy 2024
- Aircraft Location [CZDJ]
- Wing
- Aircraft Mission Design Series [CZEK]
- C130j
- Material Thickness [ABPX]
- 0.064 Inches Nominal
- End Item Identification [AGAV]
- Aircraft C130 J
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Freight Information 1560-01-433-5200
1560-01-433-5200 has freight characteristics managed by the Bureau of Accounts.. 1560-01-433-5200 has a variance between NMFC and UFC when transported by rail and the description should be consulted.