Premium Information is available for this item - Upgrade for $1 a day
1680-01-601-5802
Aircraft Interior Lining Panel
1680016015802 016015802 3350301-2
A preformed metallic/nonmetallic item specifically designed for mounting on the inside of the fuselage of an aircraft. It is of a special size, shape, and thickness to conform to the contour of the aircraft. It conceals cavities, controls, tubing, wiring and the like, as well as provides a sound barrier. Pockets, trays or shelves may be included. Excludes: PANEL, STRUCTURAL, AIRCRAFT. View more Aircraft Interior Lining Panel
January 2023
2
Marketplace 1680-01-601-5802
Request a Quotation from participating marketplace vendors
Related Documents 1680-01-601-5802 1+ Documents (More...)
RQST NE Updated Every Day 1680-01-601-5802 RQST Updated Every Day 1680-01-601-5802 RQST NE Restrictions
1680-01-601-5802 DEMIL: A | DEMILI : 1 | CRITICALITY : | HMIC : N | PMIC : A | EDC: A | ADPEC : 0 1680
Restrictions 1680-01-601-5802
1680-01-601-5802 is a Aircraft Interior Lining Panel Demilitarization of this item has been confirmed and is not currently subject to changes. 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 is not suspected to be hazardous. This item does not contain a precious metal.
Import and Export 1680-01-601-5802
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 1680-01-601-5802
- Australia (ZA01)
- Effective Date:
- 1 Jan 2012
Approved Sources 1680-01-601-5802
- Part Number
- Manufacturer
- Status
- 3350301-2
- Manufacturer
- 98897 - Lockheed Martin Corp (Active)
- Primary Buy
- Primary Buy
Similar Supply Items to 1680-01-601-5802
Freight Information 1680-01-601-5802
1680-01-601-5802 has freight characteristics managed by Australia.. 1680-01-601-5802 has a variance between NMFC and UFC when transported by rail and the description should be consulted.