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1560-01-444-6102
Aircraft Structural Panel
1560014446102 014446102 374444-1
A preformed item of various shapes, and contours, which may have a sandwich or honeycomb core bonded to a metallic or nonmetallic facing material. It is used to enclose integral portions of the fuselage or to form partitions or sections within a wing, empennage, fuselage, nacelle or crew compartment. It may have mounting provisions such as predrilled holes to facilitate installation, but will have no items attached to it except bracket (s) or other securing devices to accommodate its own mounting or support. It may be mounted by means of fasteners, bonding or welding. Excludes PANEL, INTERIOR LINING, AIRCRAFT; COVER ACCESS; COVER, ACCESS, AIRCRAFT; FLOOR (1), AIRCRAFT; CORE MATERIAL, CELLULAR, STRUCTURAL. View more Aircraft Structural Panel
January 2023
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United States (US) 4. 1560-01-444-6102 Marketplace Restrictions Approved Sources Datasheet Management
Every Day 1560-01-444-6102 RQST Updated Every Day 1560-01-444-6102 RQST NE Restrictions 1560-01-444-
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Restrictions 1560-01-444-6102
1560-01-444-6102 is a Aircraft Structural Panel 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 1560-01-444-6102
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 1560-01-444-6102
- Canada (ZC01)
- Effective Date:
- 1 Jun 2012
- Republic of Korea (ZH01)
- Effective Date:
- 1 Nov 2002
- United Kingdom (ZK01)
- Effective Date:
- 1 May 1997
Approved Sources 1560-01-444-6102
- Part Number
- Manufacturer
- Status
- 374444-1
- Manufacturer
- 98897 - Lockheed Martin Corp (Active)
- Primary Buy
- Primary Buy
Datasheet 1560-01-444-6102
- Characteristic
- Specifications
- FIIG
- Specifications
- A11700
- Material [MATT]
- Aluminum Alloy 2024
- Material Document And Classification [MDCL]
- Qq-A-362 Cond-T3 Fed Spec Single Material Response
- Aircraft Location [CZDJ]
- Aft Floor, Pilot's And Copiolt's
- Aircraft Mission Design Series [CZEK]
- C130-J
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Freight Information 1560-01-444-6102
1560-01-444-6102 has freight characteristics managed by the Bureau of Accounts.. 1560-01-444-6102 has a variance between NMFC and UFC when transported by rail and the description should be consulted.