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1560-00-185-8962

Aircraft Rudder

1560001858962 001858962 175870

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

1560-00-185-8962 RUDDER,AIRCRAFT 1560001858962 001858962

Managed by United States
NSN Created on 1 Jan 1963
Data Last Changed
January 2023
NATO Update Count
20
NATO Data Quality
1560-00-185-8962 RUDDER,AIRCRAFT 1560001858962 001858962 1/1
NSN 1560-00-185-8962 (Generic Image) 1/1

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United States (US) 4. 1560-00-185-8962 Marketplace Restrictions Approved Sources Datasheet Management
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1560-00-185-8962 Demil Restrictions 1560-00-185-8962

DEMIL: B | DEMILI: | CRITICALITY: X | HMIC: P | PMIC: U | EDC: | ADPEC:

1560-00-185-8962 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 is a US Munitions List Item and must be mutilated to scrap. 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. The precious metals content of this item is unknown.

1560-00-185-8962 HTS and ScheduleB Import and Export 1560-00-185-8962

1560-00-185-8962 End Users End Users 1560-00-185-8962

Canada (ZC01)
Effective Date:
1 Apr 1991
Portugal (ZP01)
Effective Date:
1 Apr 1991
Greece (ZU01)
Effective Date:
1 Apr 1991

1560-00-185-8962 Manufacturers Approved Sources 1560-00-185-8962

1560-00-185-8962 Technical Data Datasheet 1560-00-185-8962

Characteristic
Specifications
FIIG
A11500
Aircraft Mission Design Series [CZEK]
T-33A

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1560-00-185-8962 Freight Data Freight Information 1560-00-185-8962

1560-00-185-8962 has freight characteristics.. 1560-00-185-8962 has a variance between NMFC and UFC when transported by rail and the description should be consulted.