1420-01-330-0395
Airframe Structural Panel
1420013300395 013300395 914914-120
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 1420013300395 914914-120 A preformed item which may be any shape, having a
Restrictions 1420-01-330-0395
Import and Export 1420-01-330-0395
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 1420-01-330-0395
- MOE Rule:
- WN01
- Effective Date:
- 1 Nov 1998
- Canada (ZC01)
- Effective Date:
- 1 Apr 1991
Approved Sources 1420-01-330-0395
- Part Number
- Manufacturer
- Status
- 914914-120
- Manufacturer
- 98897 - Lockheed Martin Corp (Active)
- Primary Buy
- Primary Buy
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Freight Information 1420-01-330-0395
1420-01-330-0395 has freight characteristics managed by Canada.. 1420-01-330-0395 has a variance between NMFC and UFC when transported by rail and the description should be consulted.