1560-01-261-5188

Aircraft Rudder

1560012615188 012615188 DAA3150A681-024 DAA3150A681-002 DAA3150A681-010 DAA3150A681-018

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

1560-01-261-5188 RUDDER,AIRCRAFT 1560012615188 012615188

Managed by United States
NSN Created on 14 Aug 1987
Data Last Changed
November 2023
NATO Update Count
10
NATO Data Quality
1560-01-261-5188 RUDDER,AIRCRAFT 1560012615188 012615188 1/1
NSN 1560-01-261-5188 (Generic Image) 1/1

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1560-01-261-5188 Related Documents Related Documents 1560-01-261-5188 1+ Documents (More...)

DAA3150A681-024 DAA3150A681-002 DAA3150A681-010 DAA3150A681-018 A hinged or pivoted vertical control
United States (US) 4. 1560-01-261-5188 Marketplace Restrictions Approved Sources Datasheet Management
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1560-01-261-5188 Demil Restrictions 1560-01-261-5188

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

1560-01-261-5188 is a Aircraft Rudder that is specifically designed to be or selected as being nuclear hard. In addition it has other critical features such as tolerance, fit restrictions 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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