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4730-01-504-1925
Tube Fitting Socket Welded Ferrule
4730015041925 015041925 17P2D1098-1
A flanged cylindrical metallic item designed to be slipped over tubing and welded in place. The rear face of the flange forms a bearing surface for the coupling nut, and the front face is of a contour designed to seat against a mating contour on a fitting. When assembled the joint seals at the seat in a manner similar to a seat type union. View more Tube Fitting Socket Welded Ferrule
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Related Documents 4730-01-504-1925 5+ Documents (More...)
Tube Fitting Socket Welded Ferrule 015041925 RQST NE Updated Every Day 4730-01-504-1925 RQST Updated
Every Day 4730-01-504-1925 RQST NE Related Documents 4730-01-504-1925 5+ Documents ( More... ) https
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Tube Fitting Socket Welded Ferrule 015041925 -1 A flanged cylindrical metallic item designed https
Tube Fitting Socket Welded Ferrule 015041925 4730-14-523-5689 Socket Welded Ferrule 015041925 5918
7431 Tube Fitting Socket Welded Ferrule 144487431 01-504-1925 Tube Fitting Socket Welded Ferrule 015041925
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Fitting Socket Welded 550-4270 4730-14- -7437 4730-14-479-1831 4730-14-414-6620 4730-14-554-5918 015041925
Restrictions 4730-01-504-1925
4730-01-504-1925 is a Tube Fitting Socket Welded Ferrule 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 4730-01-504-1925
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 4730-01-504-1925
- US Air Force (FBB5)
- Effective Date:
- 1 Jan 2003
Approved Sources 4730-01-504-1925
- Part Number
- Manufacturer
- Status
- 17P2D1098-1
- Manufacturer
- 88277 - The Boeing Company (Active)
- Primary Buy
- Primary Buy
Datasheet 4730-01-504-1925
- Characteristic
- Specifications
- FIIG
- Specifications
- T385-J
- Hose/Tube Outside Diameter For Which Designed [CPMS]
- 2.040 Inches Nominal
- End Item Identification [AGAV]
- C-17A Aircraft
- Material [MATT]
- Titanium Alloy
- Part Name Assigned By Controlling Agency [CXCY]
- Ferrule,Coupling Shroud-Inerting,Air Refuel Manifold
- Overall Length [ABHP]
- 2.350 Inches Nominal
Management Data 4730-01-504-1925
- Effective Date
- Organization
- Unit of Issue
- Unit Price
- Qty Unit Pack
- Unit of Issue
- May 2010
- Department of the Air Force (DF)
- EA
- Subscribe
- 1
- EA
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Freight Information 4730-01-504-1925
4730-01-504-1925 has freight characteristics.. 4730-01-504-1925 has a variance between NMFC and UFC when transported by rail and the description should be consulted.