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1420-01-302-6356
Guided Missile Fin
1420013026356 013026356 40A13450-5
A movable airfoil, forming a part and/or all of the main directional control surfaces of a missile. It is usually perpendicular or approximately perpendicular to the longitudinal axis of the missile. Its function is to maintain uniformity of direction and to aid in the control of yaw, pitch, and roll of a guided missile in flight. View more Guided Missile Fin
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January 2023
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United States (US) 4. 1420-01-302-6356 Marketplace Restrictions Approved Sources Datasheet Management
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Restrictions 1420-01-302-6356
1420-01-302-6356 is a Guided Missile Fin that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. This item a security classified item on the US Munitions List and demilitarization is required. This item is not suspected to be hazardous. This item does not contain a precious metal.
Import and Export 1420-01-302-6356
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 1420-01-302-6356
- MOE Rule:
- WN01
- Effective Date:
- 1 Nov 1998
Approved Sources 1420-01-302-6356
- Part Number
- Manufacturer
- Status
- 40A13450-5
- Manufacturer
- 15090 - Raytheon Company (Active)
- Primary Buy
- Primary Buy
- 40A13450-5
- 14170 - Hughes Missile Systems Co San Diego (Replaced)
- Original Design
- Original Design
Datasheet 1420-01-302-6356
- Characteristic
- Specifications
- FIIG
- Specifications
- A512Z0
- End Item Identification [AGAV]
- Pacer Special
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Freight Information 1420-01-302-6356
1420-01-302-6356 has freight characteristics.. 1420-01-302-6356 has a variance between NMFC and UFC when transported by rail and the description should be consulted.