1420-01-337-7781
Airframe Structural Panel
1420013377781 013377781 276476-6
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
January 2023
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Import and Export 1420-01-337-7781
- Schedule B
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- HTS Code
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End Users 1420-01-337-7781
- MOE Rule:
- WN01
- Effective Date:
- 1 Nov 1998
- United Kingdom (ZK01)
- Effective Date:
- 1 Feb 1996
Approved Sources 1420-01-337-7781
- Part Number
- Manufacturer
- Status
- 276476-6
- Manufacturer
- 50842 - Transequip Inc (Obsolete)
- Original Design
- Original Design
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Freight Information 1420-01-337-7781
1420-01-337-7781 has freight characteristics managed by the United Kingdom (UK).. 1420-01-337-7781 has a variance between NMFC and UFC when transported by rail and the description should be consulted.