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1560-01-419-3717
Aircraft Rudder
1560014193717 014193717 16T7303-817
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
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Related Documents 1560-01-419-3717 2+ Documents (More...)
United States (US) 4. 1560-01-419-3717 Marketplace Restrictions Approved Sources Datasheet Management
RQST NE Updated Every Day 1560-01-419-3717 RQST Updated Every Day 1560-01-419-3717 RQST NE Restrictions
Aircraft Rudder 1560014193717 014193717 for $1 a day Upgrade your Account Upgrade 1560-01-419-3717Aircraft
Rudder1560014193717 014193717 16T7303 Restrictions 1560-01-500-3518 DEMIL: Q | DEMILI : 3 | CRITICALITY
Restrictions 1560-01-419-3717
1560-01-419-3717 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 considered a low risk when released from the control of the Department of Defense. The item may still be subject to the requirements of the Export Administration Regulations (EAR) and the Code of Federal Regulations (CFR). 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 1560-01-419-3717
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 1560-01-419-3717
- US Air Force (FMSU)
- Effective Date:
- 1 Sep 1995
Approved Sources 1560-01-419-3717
- Part Number
- Manufacturer
- Status
- 16T7303-817
- Manufacturer
- 81755 - Lockheed Martin Corporation (Active)
- Primary Buy
- Primary Buy
Datasheet 1560-01-419-3717
- Characteristic
- Specifications
- FIIG
- Specifications
- A11500
- Aircraft Location [CZDJ]
- Vertical Stabilizer
- Aircraft Mission Design Series [CZEK]
- F-16
- Material [MATT]
- Aluminum Alloy
Management Data 1560-01-419-3717
- Effective Date
- Organization
- Unit of Issue
- Unit Price
- Qty Unit Pack
- Unit of Issue
- Sep 1995
- Department of the Air Force (DF)
- EA
- Subscribe
- 1
- EA
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Freight Information 1560-01-419-3717
1560-01-419-3717 has freight characteristics.. 1560-01-419-3717 has a variance between NMFC and UFC when transported by rail and the description should be consulted.