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1420-01-660-8872
Guided Missile Wing Assembly
1420016608872 016608872 VP040628
An aeronautical structure designed to maintain a guided missile in stable flight. It consists of all panels, sections, fastening devices, chords,and spars, necessary for a complete wing assembly. It may or may not have plumbing accessories and/or electrical components. May include control surfaces and/or rolleron assembly, Excludes WING PANEL (as modified) and WING SECTION (as modified). View more Guided Missile Wing Assembly
January 2023
2

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Related Documents 1420-01-660-8872 1+ Documents (More...)
United States (US) 4. 1420-01-660-8872 Marketplace Restrictions Approved Sources Datasheet Management
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Restrictions 1420-01-660-8872
1420-01-660-8872 is a Guided Missile Wing Assembly 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 is not suspected to be hazardous. This item does not contain a precious metal.
Import and Export 1420-01-660-8872
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 1420-01-660-8872
- United Kingdom (ZK01)
- Effective Date:
- 1 Feb 2017
Approved Sources 1420-01-660-8872
- Part Number
- Manufacturer
- Status
- VP040628
- Manufacturer
- 51215 - Boeing Company, The (Active)
- Primary Buy
- Primary Buy
- VP040628
- K0967 - Mbda Uk Ltd (Active)
- Secondary Buy
- Secondary Buy
Datasheet 1420-01-660-8872
- Characteristic
- Specifications
- FIIG
- Specifications
- A512Z0
- Part Name Assigned By Controlling Agency [CXCY]
- Wing,Guided Missle
- Overall Width [ABMK]
- 73.0 Inches Nominal
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Freight Information 1420-01-660-8872
1420-01-660-8872 has freight characteristics.. 1420-01-660-8872 has a variance between NMFC and UFC when transported by rail and the description should be consulted.