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1560-00-994-2288
Aircraft Rudder
1560009942288 009942288 251CS10006-1
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
January 2023
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Related Documents 1560-00-994-2288 1+ Documents (More...)
RQST NE Updated Every Day 1560-00-994-2288 RQST Updated Every Day 1560-00-994-2288 RQST NE Restrictions
1560-00-994-2288 DEMIL: B | DEMILI : | CRITICALITY : X | HMIC : P | PMIC : A | EDC: | ADPEC : 0 1560
Restrictions 1560-00-994-2288
1560-00-994-2288 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. This item does not contain a precious metal.
Import and Export 1560-00-994-2288
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 1560-00-994-2288
- Greece (ZU01)
- Effective Date:
- 1 Apr 1991
Approved Sources 1560-00-994-2288
- Part Number
- Manufacturer
- Status
- 251CS10006-1
- Manufacturer
- 26512 - Northrop Grumman Systems Corporation (Active)
- Primary Buy
- Primary Buy
Datasheet 1560-00-994-2288
- Characteristic
- Specifications
- FIIG
- Specifications
- A11500
- Aircraft Mission Design Series [CZEK]
- U-16
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Freight Information 1560-00-994-2288
1560-00-994-2288 has freight characteristics.. 1560-00-994-2288 has a variance between NMFC and UFC when transported by rail and the description should be consulted.