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1730-01-499-4951
Fuselage Jacking Pad
1730014994951 014994951 5HG90213-113
An item constructed of the required shape or contour with a padding material cemented or riveted to its surface. Used for jacking of fuselage without the aid of integral jacking point. View more Fuselage Jacking Pad
January 2023
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Marketplace 1730-01-499-4951
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Related Documents 1730-01-499-4951 1+ Documents (More...)
United States (US) 4. 1730-01-499-4951 Marketplace Restrictions Approved Sources Datasheet Management
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Restrictions 1730-01-499-4951
1730-01-499-4951 is a Fuselage Jacking Pad that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. Demilitarization of this item has been confirmed and is not currently subject to changes. 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 is not suspected to be hazardous. This item does not contain a precious metal.
Import and Export 1730-01-499-4951
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 1730-01-499-4951
- US Air Force (FLL5)
- Effective Date:
- 1 Jul 2002
Approved Sources 1730-01-499-4951
- Part Number
- Manufacturer
- Status
- 5HG90213-113
- Manufacturer
- 81205 - The Boeing Company (Active)
- Primary Buy
- Primary Buy
Datasheet 1730-01-499-4951
- Characteristic
- Specifications
- FIIG
- Specifications
- T244-F
- End Item Identification [AGAV]
- F-22 Raptor
- Part Name Assigned By Controlling Agency [CXCY]
- Pad
Management Data 1730-01-499-4951
- Effective Date
- Organization
- Unit of Issue
- Unit Price
- Qty Unit Pack
- Unit of Issue
- Jul 2002
- Department of the Air Force (DF)
- EA
- Subscribe
- 1
- EA
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Freight Information 1730-01-499-4951
1730-01-499-4951 has freight characteristics.. 1730-01-499-4951 has a variance between NMFC and UFC when transported by rail and the description should be consulted.