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3040-01-564-2671
Shouldered Shaft
3040015642671 015642671 17P1C2119-1
A shaft having two or more different diameters (greater than 0.031 inches (0.79 millimeter)) along its length. It must have one or more of the following conditions: a specified surface finish designation in the range 1 to 125 microinches (0.025 to 3.2 micrometers) arithmetical average (AA), machined peripheral flat(s), circular groove(s), keyway(s), splines, threads, or holes. The ends and/or shoulders may be machined to accommodate bearings, couplings, and the like. It is not designed for use in aligning by fitting into corresponding holes of another item. For items used to support rotating members see AXLE(1), SHOULDERED. For items not having any of the above conditions see PIN, SHOULDER, HEADLESS. Excludes SHAFT(1), STRAIGHT; and AXLE(1), STRAIGHT. View more Shouldered Shaft
January 2023
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Shouldered Shaft 3040015642671 015642671 Assembly,Metal,Aft,Door,NlgSpecial Features [FEAT]Used
Restrictions 3040-01-564-2671
3040-01-564-2671 is a Shouldered Shaft that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. This item has been confirmed as a Critical Munitions List Item or a Sensitive Commerce Control List Item and cannot be in the possession of any party anywhere in the World who is not an authorized NATO Government. Any other possessor of this item should mutilate it now as possession violates international and local laws. This item is a confirmed Commerce Control List Item (CCLI). This item is not suspected to be hazardous. This item does not contain a precious metal.
Import and Export 3040-01-564-2671
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 3040-01-564-2671
- US Air Force (FBB5)
- Effective Date:
- 1 Jun 2008
Approved Sources 3040-01-564-2671
- Part Number
- Manufacturer
- Status
- 17P1C2119-1
- Manufacturer
- 88277 - The Boeing Company (Active)
- Primary Buy
- Primary Buy
Datasheet 3040-01-564-2671
- Characteristic
- Specifications
- FIIG
- Specifications
- A23200
- End Item Identification [AGAV]
- C-17A Aircraft
- First End Hole Diameter [AMDX]
- 1.0439 Inches Minimum And 1.0539 Inches Maximum
- First End Distance From End To Groove [AMCY]
- 0.7000 Inches Nominal
- First End Style [AAGZ]
- Circular Grooved
- Material [MATT]
- Aluminum Alloy 7075
- Second End Diameter [AMFZ]
- 0.7500 Inches Nominal
- Second End Style [AAHP]
- Cross Drilled Hole And Internally Threaded
- Overall Length [ABHP]
- 23.700 Inches Nominal
- Part Name Assigned By Controlling Agency [CXCY]
- Tube Assembly,Metal,Aft,Door,Nlg
- Special Features [FEAT]
- Used In Repair Of Ref Nbr 17P1c0905-503,Nsn 1620-01-490-3893 And Ref Nbr 17P1c0905-507,Nsn1620-01-505-7509 Nlg
Management Data 3040-01-564-2671
- 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
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Freight Information 3040-01-564-2671
3040-01-564-2671 has freight characteristics.. 3040-01-564-2671 has a variance between NMFC and UFC when transported by rail and the description should be consulted.