1420-01-337-7776
Airframe Structural Panel
1420013377776 013377776 276351-1
A preformed item which may be any shape, having a sandwich or honeycomb core bonded to a metallic or nonmetallic facing material. It is used to enclose any portion of the fuselage or to fabricate partitions or compartments within a wing, empennage, fuselage or nacelle. It may have holes drilled or cut to accommodate items, but will have no items mounted on it, except bracket(s) or other facilities for its own mounting or support. It may be mounted by fasteners, bonding, or welding. Excludes COVER, ACCESS; FLOOR (1), AIRCRAFT; CORE MATERIAL, CELLULAR, STRUCTURAL; COVER, ACCESS, GUIDED MISSILE; PANEL, STRUCTURAL, AIRCRAFT. View more Airframe Structural Panel
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Airframe Structural Panel 1420013377776 JavaScript in your web browser . 1420-01-337-7776Airframe
Structural Panel1420013377776 013377776 276351 Restrictions 5306-00-522-1486 DEMIL: A | DEMILI : 1 |
Restrictions 1420-01-337-7776
Import and Export 1420-01-337-7776
- Schedule B
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- HTS Code
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End Users 1420-01-337-7776
- MOE Rule:
- WN01
- Effective Date:
- 1 Nov 1998
- United Kingdom (ZK01)
- Effective Date:
- 1 Mar 1997
Approved Sources 1420-01-337-7776
- Part Number
- Manufacturer
- Status
- 276351-1
- Manufacturer
- 50842 - Transequip Inc (Obsolete)
- Original Design
- Original Design
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Freight Information 1420-01-337-7776
1420-01-337-7776 has freight characteristics managed by the United Kingdom (UK).. 1420-01-337-7776 has a variance between NMFC and UFC when transported by rail and the description should be consulted.