Premium Information is available for this item - Upgrade for $1 a day
1560-01-619-8590
Aircraft Trailing Edge
1560016198590 016198590 341801-3
The rear edge of the aileron, wing, elevator, rudder or other airfoil. It is that portion after the spar. View more Aircraft Trailing Edge
January 2023
5
Marketplace 1560-01-619-8590
Request a Quotation from participating marketplace vendors
Related Documents 1560-01-619-8590 1+ Documents (More...)
RQST NE Updated Every Day 1560-01-619-8590 RQST Updated Every Day 1560-01-619-8590 RQST NE Restrictions
1560-01-619-8590 DEMIL: Q | DEMILI : 3 | CRITICALITY : X | HMIC : P | PMIC : A | EDC: | ADPEC : 0 1560
Restrictions 1560-01-619-8590
1560-01-619-8590 is a Aircraft Trailing Edge that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. This item has been confirmed as a Critical Munitions List Item or a Sensitive Commerce Control List Item and cannot be in the possession of any party anywhere in the World who is not an authorized NATO Government. Any other possessor of this item should mutilate it now as possession violates international and local laws. This item is a confirmed Commerce Control List Item (CCLI). This item may be hazardous as it is in a Federal Supply Class for potentially hazardous items. A MSDS should be available from the supplier for the end user to evaluate any hazards. This item does not contain a precious metal.
Import and Export 1560-01-619-8590
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 1560-01-619-8590
- Australia (ZA01)
- Effective Date:
- 1 Jun 2013
Approved Sources 1560-01-619-8590
- Part Number
- Manufacturer
- Status
- 341801-3
- Manufacturer
- 98897 - Lockheed Martin Corp (Active)
- Primary Buy
- Primary Buy
Similar Supply Items to 1560-01-619-8590
Freight Information 1560-01-619-8590
1560-01-619-8590 has freight characteristics managed by Australia.. 1560-01-619-8590 has a variance between NMFC and UFC when transported by rail and the description should be consulted.