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4730-01-530-3461
Fluid Passage Bolt
4730015303461 015303461 17P6W8247-501
A boltlike item having a concentric hole along the longitudinal centerline which may extend a part or the full length of the item. It has a hole(s) perpendicular to the axis, joining or passing through the concentric hole along the longitudinal centerline. The item is designed to distribute fluid, air, or lubricant through its body to a mating item, such as a CONNECTOR, MULTIPLE, FLUID PRESSURE LINE, bearing(s), bushing(s), or the like. The item must be capable of attaching to a block fitting and/or a tubing line or be designed to accommodate a FITTING, LUBRICATION. Excludes BOLT, INTERNALLY RELIEVED BODY; BLEEDER VALVE, HYDRAULIC SYSTEM; and BUSHING, MACHINE THREAD. See also PIN, VEHICULAR LEAF SPRING SHACKLE. View more Fluid Passage Bolt
January 2023
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Restrictions 4730-01-530-3461
4730-01-530-3461 is a Fluid Passage Bolt 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 4730-01-530-3461
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 4730-01-530-3461
- US Air Force (FBB5)
- Effective Date:
- 1 May 2005
- Canada (ZC01)
- Effective Date:
- 1 Mar 2011
- NATO Maintenance and Supply Agency (ZX01)
- Effective Date:
- 1 Jan 2014
Approved Sources 4730-01-530-3461
- Part Number
- Manufacturer
- Status
- 17P6W8247-501
- Manufacturer
- 88277 - The Boeing Company (Active)
- Primary Buy
- Primary Buy
Datasheet 4730-01-530-3461
- Characteristic
- Specifications
- FIIG
- Specifications
- A121A0
- Material [MATT]
- Nickel Alloy
- Overall Length [ABHP]
- 2.500 Inches Nominal
- Special Features [FEAT]
- Drawing Name Bolt, Shoulder-Control Surface
- Supplementary Features [SUPP]
- Diameter 1.250
- End Item Identification [AGAV]
- C17a Aircraft
Management Data 4730-01-530-3461
- Effective Date
- Organization
- Unit of Issue
- Unit Price
- Qty Unit Pack
- Unit of Issue
- Nov 2018
- Department of the Air Force (DF)
- EA
- Subscribe
- 1
- EA
Air Force
- Budget:
- S
- 57X3010 - Aircraft Replenishment Spares
- Aggregation Code:
- BA
- C-17 PROGRAM
- Price Validation Code:
- E
- The current standard price is an estimated price.
Estimated Price challenges are allowed but follow procedures in para 60.b. (3) of section L of this manual.
This code will be changed to a P code upon notification of a contract price or this code will be changed to an updated code upon determination of a valid price.
- Expendability
Recoverability
Repairability: - P
- Expendable. Reparable. Condemn at Intermediate. Stock Fund (except Munitions).
NATO Stock Numbers Related to 4730-01-530-3461
Freight Information 4730-01-530-3461
4730-01-530-3461 has freight characteristics.It has a National Motor Freight Classification (NMFC) of 052250. A Sub NMFC of X. It has a NMFC Description of PIPE R TUBING R PIPE FITTINGS NOI. 4730-01-530-3461 is rated as class 70 when transported by Less-Than Truckload (LTL) freight. It has a Uniform Freight Classification (UFC) number of 30215 which rates the freight between FCL and LCL. 4730-01-530-3461 has a variance between NMFC and UFC when transported by rail and the description should be consulted. It has a Water Commodity Code (WCC) of 846 for ocean manifesting and military sealift. 4730-01-530-3461 is not classified as a special type of cargo when transported by water. 4730-01-530-3461 is not a consolidation and does not exceed 84" in any dimension. It should be compatible with a standard 72" Aircraft Cargo Door when transported by air.