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5307-00-419-2951
Stepped Stud
5307004192951 004192951 54751P006
A headless fastener not exceeding 12 inches (304.8 mm) in length, threaded externally on both ends on which the nominal diameter of one threaded section is greater than the other. The entire unthreaded portion must be of a single diameter equal to or smaller than the maximum major diameter of the larger threaded end. Includes radial grooves or thread reliefs. Excludes items with tapered threads. View more Stepped Stud
January 2023
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Marketplace 5307-00-419-2951
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Restrictions 5307-00-419-2951
5307-00-419-2951 is a Stepped Stud 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. The precious metals content of this item is unknown.
End Users 5307-00-419-2951
- Brazil (YA01)
- Effective Date:
- 1 May 2012
- Republic of Korea (ZH01)
- Effective Date:
- 1 Apr 1991
Approved Sources 5307-00-419-2951
- Part Number
- Manufacturer
- Status
- 54751P006
- Manufacturer
- 63005 - Rolls-Royce Corporation (Active)
- Primary Buy
- Primary Buy
- 54751P006
- 73342 - Allison Transmission Inc (Active)
- Canceled/Obsolete
- Canceled/Obsolete
Datasheet 5307-00-419-2951
- Characteristic
- Specifications
- FIIG
- Specifications
- A051A0
- Distance From Cotter Pin Hole Centerline To Nut End [ADDU]
- 0.131 Inches Minimum First Hole And 0.151 Inches Maximum First Hole
- Cotter Pin Hole Diameter [ADDV]
- 0.060 Inches Minimum First Hole And 0.080 Inches Maximum First Hole
- Hardness Rating [CQFM]
- 26.0 Rockwell C Minimum And 32.0 Rockwell C Maximum
- Material [MATT]
- Steel
- Nominal Thread Size [CQJX]
- 0.250 Inches Nut Thread
- Nominal Thread Size [CQJX]
- 0.312 Inches Stud Thread
- Material Document And Classification [MDCL]
- Ems 85045,Fscm 24617 Mfr Ref Single Material Response
- Shank Diameter [AAZE]
- 0.246 Inches Minimum And 0.249 Inches Maximum
- Overall Length [ABHP]
- 1.521 Inches Minimum And 1.541 Inches Maximum
- Style Designator [STYL]
- Stepped
- Surface Finish [CSYM]
- 63.0 Microinches Overall
- Thread Class [AAJD]
- 3A Nut Thread
- Thread Direction [AAJF]
- Right-Hand Nut Thread
- Thread Direction [AAJF]
- Right-Hand Stud Thread
- Thread Length [AASA]
- 0.490 Inches Minimum Nut Thread And 0.510 Inches Maximum Nut Thread
- Thread Length [AASA]
- 0.490 Inches Minimum Stud Thread And 0.510 Inches Maximum Stud Thread
- Thread Pitch Diameters [AAJE]
- +0.2839/+0.2854 Inches Stud Thread
- Thread Quantity Per Inch [CMLP]
- 18 Stud Thread
- Thread Quantity Per Inch [CMLP]
- 28 Nut Thread
- Thread Series Designator [THSD]
- Unf Nut Thread
- Thread Series Designator [THSD]
- Uns Stud Thread
NATO Stock Numbers Related to 5307-00-419-2951
Freight Information 5307-00-419-2951
5307-00-419-2951 has freight characteristics managed by Germany.It has a National Motor Freight Classification (NMFC) of 093486. A Sub NMFC of Z. It has a NMFC Description of BOLTS,NUTS OR SCREWS, NOI (SUB 3). 5307-00-419-2951 is rated as a variable freight class when transported by Less-Than Truckload (LTL) freight. 5307-00-419-2951 is rated as class 50 when transported by Less-Than Carload (LCL) rail or ocean freight. It has a Uniform Freight Classification (UFC) number of 48950 which rates the freight between FCL and LCL. 5307-00-419-2951 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 573 for ocean manifesting and military sealift. 5307-00-419-2951 is not classified as a special type of cargo when transported by water. 5307-00-419-2951 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.