1560-01-419-4355

Aircraft Rudder

1560014194355 014194355 DAA3150A681-044

A hinged or pivoted vertical control surface, usually hinged to the tail post aft of the vertical stabilizer, for the purpose of applying yawing moments to an aircraft to assist in initiating right or left turns about the vertical axis of flight. It may include a trim tab mechanism. Excludes STABILIZER, VERTICAL. View more Aircraft Rudder

1560-01-419-4355 RUDDER,AIRCRAFT 1560014194355 014194355

Managed by United States
NSN Created on 21 Sep 1995
Data Last Changed
November 2023
NATO Update Count
3
NATO Data Quality
1560-01-419-4355 RUDDER,AIRCRAFT 1560014194355 014194355 1/1
NSN 1560-01-419-4355 (Generic Image) 1/1

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DAA3150A681-044 A hinged or pivoted vertical control surface, usually hinged to the tail post aft of
United States (US) 4. 1560-01-419-4355 Marketplace Restrictions Approved Sources Datasheet Management
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1560-01-419-4355 Demil Restrictions 1560-01-419-4355

DEMIL: P | DEMILI: | CRITICALITY: X | HMIC: P | PMIC: A | EDC: | ADPEC: 0

1560-01-419-4355 is a Aircraft Rudder 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 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.

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